The Online Books Page

Online Books by

Air Force Flight Dynamics Laboratory (U.S.)

Books from the extended shelves:

• Air Force Flight Dynamics Laboratory (U.S.): 3-D composite velocity solutions for subsonic/transonic flow over forebodies and afterbodies (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Research Development Center, Air Force Systems Command, United States Air Force, 1989., 1989), also by Raymond E. Gordnier, Inc Universal Energy Systems, Wright Research and Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A-10 static structural test program (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by Thomas F. Hughes, Frederick E. Hussong, Martin D. Richardson, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Active flutter suppression on an aeroelastically tailored HiMAT vehicle (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by John H. Wykes, United States. Air Force. Systems Command, and Rockwell International. Los Angeles Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Adaptive control of wing/store flutter (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by C. A. Harvey, G. Stein, T. L. Johnson, Air Force Wright Aeronautical Laboratories, and Honeywell Systems and Research Center (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An adaptive grid algorithm for nonequilibrium hypersonic flows (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Research and Development Center, Air Force Systems Command, United States Air Force, 1990., 1990), also by Michael John Aftosmis, Judson R. Baron, Massachusetts Institute of Technology. Department of Aeronautics and Astronautics, Wright Research and Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Additional research of low altitude turbulence data : final report (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by Joe D. Gault, Boeing Company. Wichita Division, and LO-LOCAT program (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Adhesive strip concept for delamination arrestment (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1986., 1986), also by James R. Eisenmann, David A. Ulman, Air Force Wright Aeronautical Laboratories, and General Dynamics Corporation. Fort Worth Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Advanced ejection seat for high dynamic pressure escape wind tunnel test report (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by J. O. Bull, R. F. Yurczyk, D. T. Ther, Air Force Wright Aeronautical Laboratories, and Boeing Military Airplane Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Advanced electromechanical actuation system (EMAS) development and flight test (C-141 aircraft) demonstration (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1988., 1988), also by T. Mark Bailey, K. C. Thompson, Air Force Wright Aeronautical Laboratories, Sundstrand Corporation, and Lockheed Aeronautical Systems Company. Georgia Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Advanced fatigue damage development in graphite epoxy laminates (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by Russell D. Jamison, K. L. Reifsnider, Air Force Wright Aeronautical Laboratories, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Advanced Fighter Technology Integration (AFTI) Phase I. Volume II Part II, Appendix I, Phase I wind tunnel data summary (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1975., 1975), also by Gordon Rosenthal and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Advanced residual strength degradation rate modeling for advanced composite structures. Volume 1. Task I: Preliminary screening (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by D. E. Pettit, J. M. Cox, K. N. Lauraitis, Air Force Wright Aeronautical Laboratories, and Lockheed-California Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Advanced residual strength degradation rate Modeling for advanced composite structures. Volume 2. Tasks II and III (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by K. N. Lauraitis, D. E. Pettit, J. T. Ryder, Air Force Wright Aeronautical Laboratories, and Lockheed-California Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Advanced residual strength degradation rate modeling for advanced composite structures. Volume 3. Appendixes to report for Tasks II and III (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by K. N. Lauraitis, D. E. Pettit, J. T. Ryder, Air Force Wright Aeronautical Laboratories, and Lockheed-California Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aeroacoustic environment of a store in an aircraft weapons bay (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratroy, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by L. L. Shaw, D. L. Smith, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aerodynamic analysis of a fighter aircraft with a higher order paneling method (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by A. R. Dusto, Air Force Wright Aeronautical Laboratories, and Boeing Military Airplane Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aerodynamic characteristics and flap loads for a blunt pyramidal configuration at Mach 5 and 8 : part of an investigation of hypersonic flow separation and control characteristics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by William J. Evans, United States. Air Force. Systems Command, and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aerodynamic characteristics of non-straight-taper wings (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1966., 1966), also by David B. Benepe, J. Bert Webb, Bobby G. Kouri, and General Dynamics Corporation. Fort Worth Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aerodynamic configured missile development : final report. Volume I, Executive Summary (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by R. J. Krieger, M. L. Taylor, E. A. Eiswirth, R. F. Hood, J. E. Gregoire, Air Force Wright Aeronautical Laboratories, and McDonnell Douglas Astronautics Company-St. Louis (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aerodynamic configured missile development : final report. Volume II, Configuration Development. Appendix B, Relations between aerodynamic characteristics and performance (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by R. J. Krieger, M. L. Taylor, E. A. Eiswirth, R. F. Hood, J. E. Gregoire, Air Force Wright Aeronautical Laboratories, and McDonnell Douglas Astronautics Company-St. Louis (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aerodynamic configured missile development : final report. Volume II, Configuration Development. Appendix A, Aerodynamic configured missile reference library summary (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by R. J. Krieger, M. L. Taylor, E. A. Eiswirth, R. F. Hood, J. E. Gregoire, Air Force Wright Aeronautical Laboratories, and McDonnell Douglas Astronautics Company-St. Louis (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aerodynamic configured missile development : final report. Volume III, Missile aerodynamic prediction rationale using the Supersonic/Hypersonic arbitrary body program (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by R. J. Krieger, M. L. Taylor, E. A. Eiswirth, R. F. Hood, J. E. Gregoire, Air Force Wright Aeronautical Laboratories, and McDonnell Douglas Astronautics Company-St. Louis (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aerodynamic configured missile development : final report. Volume IV, Phase I experimental program (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by R. J. Krieger, D. S. Gillies, M. L. Taylor, E. A. Eiswirth, R. F. Hood, J. E. Gregoire, Air Force Wright Aeronautical Laboratories, and McDonnell Douglas Astronautics Company-St. Louis (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aerodynamic configured missile development final report. Volume V, Phase II experimental program (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by R. J. Krieger, D. S. Gillies, M. L. Taylor, E. A. Eiswirth, R. F. Hood, J. E. Gregoire, Air Force Wright Aeronautical Laboratories, and McDonnell Douglas Astronautics Company-St. Louis (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aerodynamic configured missile development : final report. Volume VI, Phase III experimental program (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by R. J. Krieger, D. S. Gillies, M. L. Taylor, E. A. Eiswirth, R. F. Hood, J. E. Gregoire, Air Force Wright Aeronautical Laboratories, and McDonnell Douglas Astronautics Company-St. Louis (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aerodynamic Deployable Decelerator Performance-Evaluation Program : Phase 2 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technical Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by E. Bloetscher and Goodyear Aerospace Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aerodynamic improvements by discrete wing tip jets (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984, 1984), also by Zhengming Wu, Ahmad D. Vakili, Air Force Wright Aeronautical Laboratories, and University of Tennessee (System). Space Institute (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aerodynamic stability and control/wind tunnel data correlation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by G. R. Casteel and North American Rockwell Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aerodynamic stability technology for maneuverable missiles. Volume I, Configuration aerodynamic characteristics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by Gennaro F. Aiello, Michael C. Bateman, Martin Marietta Corporation, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aerodynamic stability technology for maneuverable missiles. Volume II, Asymmetric vortex effects computer program (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by Gennaro F. Aiello, Michael C. Bateman, Martin Marietta Corporation, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aerodynamic testing in a free-flight spark range (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1997., 1997), also by G. L. Winchenbach and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aeroelastic stability and performance characteristics of aircraft with advanced composite sweptforward wing structures (Wright-Patterson Air Force Base : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1978., 1978), also by Terry A. Weisshaar and Virginia Polytechnic Institute and State University. Aerospace and Ocean Engineering Department (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aerospace structures design on computers (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Research and Development Center, Air Force Systems Command, United States Air Force, 1989., 1989), also by V. B. Venkayya, Wright Research and Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aerospace vehicles (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1966), also by George Gerard and Allied Research Associates (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The AFFDL-Nielsen flow-field study (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by William T Strike, John H. Porter, Terry R. Penney, Nielsen Engineering & Research, Arnold Engineering Development Center, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Aircraft motion analysis (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by J. A. Thelander, United States. Air Force. Systems Command, and Douglas Aircraft Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Airplane flying characteristics in turbulence (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by E. D. Onstott, E. P. Salmon, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Algorithms for zonal methods and development of three dimensional mesh generation procedures (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984, 1984), also by Joseph L. Steger, Air Force Wright Aeronautical Laboratories, and Stanford University. Department of Aeronautics and Astronautics (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Allowable stresses for elevated temperature structures (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by C. G. Swanson, P. C. Huang, C. J. Van der Maas, United States. Air Force. Systems Command. Aeronautical Systems Division, and Martin Marietta Corporation. Baltimore Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Analysis and control of grid quality in computational simulation (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1992., 1992), also by J. F. Thompson, B. Gatlin, C. Wayne Mastin, Air Force Wright Aeronautical Laboratories, and Mississippi State University. Engineering Research Center (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Analysis of commercial and military STOL design criteria (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by Robert B. Smith, Alan H. Marsh, R. Sheldon Hess, Douglas Aircraft Company, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Analysis of digital flight control systems with flying qualities applications. Volume I, Executive summary (Wright-Patterson Air Force Base : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1978., 1978), also by Richard F. Whitbeck and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Analysis of digital flight control systems with flying qualities applications. Volume II, Technical report (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1978., 1978), also by Richard F. Whitbeck, L. G. Hofmann, and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An analysis of fixed wing-proprotor interference for folding proprotor aircraft (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by Carl G. Matthys, P. Y. Hsieh, Mukund M. Joglekar, United States. Air Force. Systems Command, and Bell Helicopter Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An analysis of flexible aircraft structural mode control. Part 1, Unclassified data (Wright-Patterson Air Force Base, Ohio : AF Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1966., 1966), also by John H. Wykes, Alva S. Mori, Wright-Patterson Air Force Base (Ohio), and North American Aviation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Analysis of limited authority manual control systems (Wright-Patterson AFB, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by Lee Gregor Hofmann, Dunstan Graham, Kishor V. Shah, and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Analysis of several handling quality topics pertinent to advanced manned aircraft (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967), also by Robert L. Stapleford, J. Alfred Tennant, John J. Best, Dunstan Graham, Irving L. Ashkenas, and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Analysis of structural shells with transverse shear deformation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by RIchard L. Citerley, United States. Air Force. Systems Command, and Inc Anamet Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Analysis of the influences of different parameters on a reaction jet single-axis satellite attitude control system (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by Hans-Paul Riemann (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An analysis of the stability and control characteristics of an ejector wing V/STOL during transition (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by George Kurylowich, James M. Martin, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Analysis of two nonlinear flight control systems. Part I, Liapounov-Lurje approach to a simplified pitch rate autopilot. Part II, Analysis of a high-gain adaptive pitch rate autopilot (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by T. R. Alex, C. R. Heermann, General Dynamics Corporation. Astronautics Division, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Analysis/Theory of controlled configured structures (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), also by J. G. Williams and LTV Aerospace Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An analytical approach to predict the aerodynamic stability characteristics of an autorotating ribbed spherical bomblet (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), also by David R. Mayhew (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Analytical design methods for aircraft structural joints (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by W. F. McCombs, J. L. Perry, J. C. McQueen, and LTV Aerospace Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The analytical determination of the thermal response of a typical aircraft structure subjected to transient external heating and cooling (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by Thomas N. Bernstein, Robert M. Engle, and Gene E. Maddux (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An analytical study of V/STOL handling qualities in hover and transition (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by Robert L. Stapleford and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Application of a three-dimensional steady and unsteady full potential method for transonic flow computations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984, 1984), also by J. B. Malone, N. L. Sankar, Air Force Wright Aeronautical Laboratories, and Lockheed-Georgia Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Application of optimality criterion to fiber-reinforced composites (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by N. S. Khot, V. A. Tischler, C. D. Johnson, V. B. Venkayya, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An application of the finite element method to elastic-plastic problems of plane stress (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), also by M. Salmon, R. Sandhu, L. Berke, and IIT Research Institute (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Applied heat transfer course lecture notes on interference flows (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Flight Mechanics Division, High Speed Aero Performance Branch, Air Force Systems Command, United States Air Force, 1972., 1972), also by Gerald L. Burke (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An approximate analysis of wing unsteady aerodynamics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories. Air Force Systems Command, United States Air Force, 1979., 1979), also by William R. Wells, Wright State University, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Approximate multiple configuration analysis and allocation for least weight structural design (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by Robert J. Melosh and R. Luik (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An approximate solution of unsteady transonic flow problems (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), also by Kenneth R. Kimble, Jain-Ming Wu, and University of Tennessee (System). Space Institute (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An assessment of current capability for computer analysis of shell structures (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by Richard F. Hartung and Lockheed Palo Alto Research Laboratory (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): ASTROS enhancement final report (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1995., 1995), also by David L. Herendeen, D. J. Neill, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): ASTROS enhancement Volume I. ASTROS users manual (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1993., 1993), also by D. J. Neill, David L. Herendeen, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): ASTROS enhancement Volume II. ASTROS programmer's manual (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1993., 1993), also by D. J. Neill, R. L. Hoesly, David L. Herendeen, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Asymptotic far field conditions for unsteady subsonic and transonic flows (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1983., 1983), also by Karl Gottfried Guderley, Air Force Wright Aeronautical Laboratories, and University of Dayton. Research Institute (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Automated early fatigue damage sensing system (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1988., 1988), also by Alan Hencken, Michael Horn, Air Force Wright Aeronautical Laboratories, and Northrop Grumman Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Automated method for the large deflection and instability analysis of three-dimensional truss and frame assemblies (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966), also by R. H. Mallett, L. Berke, and Case Institute of Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An automated procedure for computing the three-dimensional transonic flow over wing-body combinations, including viscous effects. Volume II, Program unser's manual and code description. Appendix A, Computer code listing and flowchart (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1977., 1977), also by William H. Mason, Juanita Frick, W. F. Ballhaus, Mark Stern, Donald Mackenzie, Grumman Aerospace Corporation, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An automated procedure for the optimization of practical aerospace structures. Volume 1, Theoretical development and user's information (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamicsl Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by Walter J. Dwyer, Irving U. Ojalvo, Robert K. Emerton, United States. Air Force. Systems Command, and Grumman Aerospace Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An automated procedure for the optimization of practical aerospace structures. Volume 2, Programmer's manual (Air Force Flight Dynamicsl Laboratory, Air Force Systems Command, United States Air Force, 1971), also by Walter J. Dwyer, Patricia L. Sabatelli, Robert K. Emerton, United States. Air Force. Systems Command, and Grumman Aerospace Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Automated structural optimization system (ASTROS). Volume I. Theoretical manual (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1988., 1988), also by E. H. Johnson, V. B. Venkayya, Air Force Wright Aeronautical Laboratories, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Automated structural optimization system (ASTROS). Volume III, Applications manual (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1988., 1988), also by E. H. Johnson, D. J. Neill, Air Force Wright Aeronautical Laboratories, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): B-66B low level gust study. Volume XI, Crew Comments. Part 2, Flights G-54-G115 (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Flight Dynamics Laboratory, Air Research and Development Command, United States Air Force, 1961., 1961), also by United States. Wright Air Development Division, United States. Air Force. Air Research and Development Command, and Douglas Aircraft Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Behavior of extraction parachutes in the wake of a powered airplane model (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by H. G. Heinrich, G. D. Hulcher, and University of Minnesota. Department of Aerospace Engineering and Mechanics (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A bibliography of recent developments in unsteady transonic flow (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1979-1980., 1979), also by Christopher J. Borland and Boeing Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Boundary layer effects : proceedings of the 7th U.S. Air Force/Federal Republic of Germany Data Exchange Agreement Meeting (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1978., 1978), also by Anthony W. Fiore, Germany (West), United States Air Force, and Ohio) U.S. Air Force/Federal Republic of Germany Data Exchange Agreement Meeting (7th : 1978 : Wright Patterson Air Force Base (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Boundary-layer stability analysis for sharp cones at zero angle-of-attack (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1986., 1986), also by Mack Leslie M., Air Force Wright Aeronautical Laboratories, and Jet Propulsion Laboratory (U.S.) (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Buckling of composites under hot and wet environment (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984., 1984), also by V. Sarma Avva, L. Sharpe, D. Yogi Goswami, Air Force Wright Aeronautical Laboratories, and North Carolina Agricultural and Technical State University (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Buckling of fiber-reinforced circular cylinders under axial compression (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by Roderick C. Tennyson, N. S. Khot, K. H. Chan, D. B. Muggeridge, University of Toronto. Institute for Aerospace Studies, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Buffet characteristics of the model F-4 airplane in the transonic flight regime (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1970., 1970), also by Marshall Cohen, McDonnell Aircraft Company, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): CADS : Computer Aided Design System. Volume I, Final summary report (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), also by Michael C. Less, Susan Manuel, Air Force Wright Aeronautical Laboratories, and Rockwell International (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Calculated values of transient and steady state performance characteristics of man-carrying, cargo, and extraction parachutes (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1966), also by Eugene L. Haak, Richard V. Hovland, Wright-Patterson Air Force Base (Ohio), and University of Minnesota (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Calculation of high angle of attack aerodynamics of fighter configurations. Vol. I, Steady (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate, Wright Laboratory, Air Force Systems Command, United States Air Force, 1991., 1991), also by C. Edward Lan, Ratikanta Tripathi, S. C. Mehrotra, P. Sundaram, Suei Chin, H. Emdad, Vigyan Research Associates, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Calculation of high angle of attack aerodynamics of fighter configurations. Vol. II, User manual for VORSTAB-II (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate, Wright Laboratory, Air Force Systems Command, United States Air Force, 1991., 1991), also by C. Edward Lan, Ratikanta Tripathi, S. C. Mehrotra, P. Sundaram, Suei Chin, H. Emdad, Vigyan Research Associates, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Calculation of high angle of attack aerodynamics of fighter configurations. Vol. III, Unsteady (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate, Wright Laboratory, Air Force Systems Command, United States Air Force, 1991., 1991), also by C. Edward Lan, Ratikanta Tripathi, S. C. Mehrotra, P. Sundaram, Suei Chin, H. Emdad, Vigyan Research Associates, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Calculation of high speed inlet flows using the Navier-Stokes equations. Volume 1, Description of results / Doyle D. Knight. (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1980., 1980), also by Doyle D. Knight and Rutgers University. Department of Mechanical & Aerospace Engineering (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Calculation of high speed inlet flows using the Navier-Stokes equations. Volume II, User's and programmer's guide (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by Doyle D. Knight, Air Force Wright Aeronautical Laboratories, and Rutgers University. Department of Mechanical & Aerospace Engineering (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The calculation of nonlinear supersonic conical flows by the method of integral relations (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by John W. Brook, United States. Air Force. Systems Command, Aeronautical Research Associates of Princeton, and Grumman Aircraft Engineering Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The calculation of three-dimensional supersonic flows around spherically-capped smooth bodies and wings (Air Force Flight Dynamics Laboratory, Air Force Systems Command, Wright-Patterson Air Force Base, 1972), also by Chong-Wei Chu, Sidney A. Powers, and Wright-Patterson Air Force Base United States. Air Force Flight Dynamics Laboratory (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A calculator program for analyzing airloads on a wing of arbitrary planform and camber in subsonic flow (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1978., 1978), also by John C. Sparks and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Cambered jet-flapped airfoil theory with tables and computer programs for application (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1977., 1977), also by Henry W. Woolard, Bernard F. Niehaus, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Cavity oscillation in cruise missile carrier aircraft (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by Harold W. Bartel, James M. McAvoy, Air Force Wright Aeronautical Laboratories, and Lockheed-Georgia Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Characterization of fatigue crack growth in bonded structures. Volume I, Crack growth prediction in bonded structures (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by M. M. Ratwani, United States. Air Force. Systems Command, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Characterization of fatigue crack growth in bonded structures. Volume II, Analysis of cracked bonded structures (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by M. M. Ratwani, United States. Air Force. Systems Command, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Collapse analysis for shells of general shape. Volume 1, Analysis (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by Bo O. Almroth, M. B. Marlowe, F. A. Brogan, and Lockheed Palo Alto Research Laboratory (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Collapse analysis for shells of general shape. Volume 2. User's manual for the STAG-A computer code (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by Bo O. Almroth, H. T. Petersen, F. Zele, E. Meller, F. A. Brogan, and Lockheed Palo Alto Research Laboratory (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Comments on hypersonic boundary-layer transition (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Research and Development Center, Air Force Systems Command, United States Air Force, 1990., 1990), also by Kenneth F. Stetson, Wright Research and Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Commercial supersonic tansport panel flutter studies (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by C. H. Hodson, J. E. Stocker, North American Aviation, United States. Federal Aviation Agency, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Compatibility of maneuver load control and relaxed static stability (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by W. J. Rohling, W. J. Wattman, L. H. Pasley, United States. Air Force. Systems Command, and Boeing Company. Wichita Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A compilation of computer programs in flight vehicle technology : 1964-1967 (Wright-Patterson Air Force Base, Ohio : Air Force Systems Command, Air Force Flight Dynamics Laboratory, 1968., 1968), also by Ambrose B. Nutt (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Compilation of data on crew emergency escape systems (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, XXXX, 1966), also by John O. Bull, Howard L. McDowell, Edward L. Serocki, and Boeing Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Composite wing design for aeroelastic requirements ([Wright-Patterson Air Force Base, Ohio] : [Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force] 1972., 1972), also by L. A. McCullers, R. W. Lynch, General Dynamics Corporation. Convair Division, United States. Air Force. Systems Command, and Ohio) Conference on Fibrous Composites in Flight Vehicle Design ([1st] : 1972 : Dayton (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Compressible boundary layer equations and stagnation point solution with differences in thermal and dynamic boundary layer thickness being considered (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Melving L. Buck and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Computation of ramjet internal flowfields (Wright-Patterson Air Force Base, Ohio : Aeropropolsion and Power Laboratory, Wright Research and Development Center, Air Force Systems Command, United States Air Force, 1989., 1989), also by James N. Scott, Thomas P. Gielda, Wilbur L. Hankey, University of Dayton, Wright Research and Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Computation of three-dimensional supersonic viscous flows in internal corners (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by John C. Tannehill, Dale A. Anderson, Air Force Wright Aeronautical Laboratories, and Inc Engineering Analysis (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Computation of viscous shock/shock hypersonic interactions with an implicit flux split scheme (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Laboratory, Air Force Systems Command, United States Air Force, 1990., 1990), also by Datta V. Gaitonde, Inc Universal Energy Systems, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Computations of the nonequilibrium flow of a viscous, radiating fluid about a blunt axisymmetric body. Volume I, Equations and Results (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by J. T. Curtis, C. R. Strom, and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Computations of the nonequilibrium flow of a viscous, radiating fluid about a blunt axisymmetric body. Volume II, Program details and operating procedure (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by J. T. Curtis, C. R. Strom, and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Computer oriented analysis of shell structures : proceedings of a conference held at Palo Alto, California, August 10-14, 1970 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by Richard F. Hartung and Lockheed Missiles and Space Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Computer program for design and/or analysis of two-dimensional and axisymmetric inlets (Wright-Patterson Air Force Base : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1979., 1979), also by Larry K. Ratliff (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Computer program to perform aircraft design synthesis. Volume II, Technical volume (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), also by B. H. Oman, T. F. Reed, N. P. Karil, S. K. Pederson, and General Dynamics Corporation. Convair Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Computer programs for calculating small disturbance transonic flows about oscillating airfoils (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), also by J. L. Farr, E. D. Albano, R. M. Traci, and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Computer rogram (OPTCOMP) for optimization of composite structures for minimum weight design (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wrigth Aeronautical Laboratories, Air Force System Command, United States Air Force, 1977., 1977), also by N. S. Khot and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Computer techniques for the rapid flutter clearance of aircraft carrying external stores. Part I, Perturbation theory and applications (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by A. K. Cross, E. A. Albano, Northrop Corporation. Aircraft Division, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Computerized data catalog and retrieval system for deployable aerodynamic decelerators (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by Thomas J. Hogan, John J. Schauer, and Technology Incorporated (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A conical thin-shock-layer theory uniformly valid in the entropy layer (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by Robert E. Melnik, United States. Air Force. Systems Command, Wright-Patterson Air Force Base. Flight Dynamics Laboratory, Aeronautical Research Associates of Princeton, and Grumman Aircraft Engineering Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Contributions to the theory of randomly forced, nonlinear, multiple-degree-of-freedom, coupled mechanical systems (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by H. L. Fox, P. R. Nayak, R. W. Pyle, P. W. Smith, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Control configured vehicle ride control system (CCV RCS) : B-52 control system analysis, synthesis, and design (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by C. R. Stockdale and R. D. Poyneer (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Control effectiveness of transverse jets interacting with a high-speed free stream. Volume I. Design charts, theoretical and experimental results (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by J. W. Barnes, H. H. Tang, J. G. Davis, and Douglas Aircraft Company. Santa Monica Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Control of orbiting large space structural systems with discrete time observational data and random measurement noise (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Research and Development Center, Air Force Systems Command, United States Air Force, 1990., 1990), also by Peter M. Bainum, Aprille Ericsson-Jackson, Guangqian Xing, Howard University. Department of Mechanical Engineering, Wright Research and Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Correlation of aerodynamic stability and control derivatives obtained from flight tests and wind tunnel tests on the XC-142A airplane (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), also by Ernest L. Black, George C. Booth, and LTV Aerospace Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Cracks, a Fortran IV digital computer program for crack propagation analysis (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), also by Robert M. Engle and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Crew escape capsule retrorocket concept. Volume I, Demonstration program (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by Marvin C. Whitney and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Crew escape concepts for advanced high performance aircraft (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1978., 1978), also by Douglas E. Swanson, United States. Air Force. Systems Command, and Boeing Aerospace Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Critical evaluation of transition from laminar to turbulent shear layers with emphasis on hypersonically traveling bodies (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), also by Mark Vladimir Morkovin and Md.) Research Institute for Advanced Study (Baltimore (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The cyclic state of materials and the relationship to mechanical properties and fatigue (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, XXXX1966., 1966), also by Dewey G. Younger (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Demonstration of a transonic box method for unsteady aerodynamics of planar wings (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1966., 1966), also by J. J. Olsen (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A description of the atmospheric turbulence environment derived from the critical atmospheric turbulence (ALLCAT) program (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by Paul L. Hasty and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Design and instrumentation of a water flow channel and application to some aerodynamics problems (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by Shukry K. Ibrahim, United States. Air Force. Systems Command, and University of Minnesota. Department of Aerospace Engineering and Mechanics (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Design criteria for rolling element air frame bearings for high temperature and high altitude use (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, [1963], 1963), also by Harold E. Munson, J. H. Johnson, Jamshed B. Havewala, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Design criteria for the future of flight controls : proceedings of the Flight Dynamics Laboratory Flying Qualities and Flight Control Symposium, 2-5 March, 1982. (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by Flight Dynamics Laboratory Flying Qualities and Flight Control Symposium (1982 : Dayton), D. W. Potts, S. G. Fuller, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Design development and durability validation of postbuckled composite and metal panels: technology assessment (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), also by Ravi B. Deo, Air Force Wright Aeronautical Laboratories, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Design method for fully augmented systems for variable flight conditions (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, AIr Force Systems Command, United States Air Force, 1972., 1972), also by Albert J. VanDierendonck, United States. Air Force. Systems Command, and Honeywell Inc. Systems and Research Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Design Methodology and Life Analysis of Postbuckled Metal and Composite Panels: Design Guide. Volume III (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Materials Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), also by Ravi B. Deo, B. L. Agarwal, Air Force Wright Aeronautical Laboratories, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Design methodology and life analysis of postbuckled metal and composite panels. Volume I (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Materials Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), also by Ravi B. Deo, Erdogan Madenci, B. L. Agarwal, Air Force Wright Aeronautical Laboratories, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Determination of moisture content in composites by dielectric measurements (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by A. O. Kays, Air Force Wright Aeronautical Laboratories, and Lockheed-Georgia Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Determination of the local heat-transfer characteristics on glaze ice accretions on a cylinder and a NACA 0012 airfoil (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1987., 1987), also by Martinho R. Pais, S. N. Singh, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Development and design criteria for a dry film lubricated bearing system (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by M. E. Campbell, J. W. Van Wyk, United States. Air Force. Systems Command. Aeronautical Systems Division, and Boeing Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The development and solution of boundary integral equations for crack problems in fracture mechanics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1976., 1976), also by L. T. Montulli and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Development and testing of a new optimum design code for hypersonic wind tunnel nozzles, including boundary layer, turbulence, and real gas effects (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1996., 1996), also by Ralph C. Tolle and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Development design methods for predicting hypersonic aerodynamic control characteristics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by Z. Popinski, C. F. Ehrlich, and Lockheed-California Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Development feasibility of missile datcom (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by Steven R. Vukelich, Air Force Wright Aeronautical Laboratories, and McDonnell Douglas Astronautics Company-St. Louis (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Development of a mathematical model for predicting the percentage fatigue life increase resulting from shot peened components. Phase I (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), also by Roger S. Simpson and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Development of a nozzle to improve the turning of supersonic Coanda jets (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by Paul M. Bevilaqua, J.D. Lee, Air Force Wright Aeronautical Laboratories, and North American Rockwell Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Development of an aeroacoustic methodology to evaluate heatshield material performance (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by A. L. Laganelli, Air Force Wright Aeronautical Laboratories, and inc Science Applications (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Development of an empirically based computer program to predict the aerodynamic characteristics of aircraft. Volume I, Empirical methods. (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by Roy T. Schemensky and General Dynamics Corporation. Convair Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Development of an empirically based computer program to predict the aerodynamic characteristics of aircraft. Volume I, Basic Theoretical methods (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by M. L. Goldhammer, C. C. Shen, M. L. Lopez, and Douglas Aircraft Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Development of experimental testing programs to verify thermal stress analysis (Wright-Patterson AIr Force Base, Ohio : Air Force Flight Dynamicas Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by B. E. Gatewood, B. H. Ulrich, A. R. Glaser, and Ohio State University. Department of Aeronautical and Astronautical Engineering (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Development of innovative air combat measures of merit for supermaneuverable fighters (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1987., 1987), also by Robert W. Foltyn, Anthony J. Arand, Orlando Laboy, Andrew M. P. Lynch, Urban H. Lynch, Andrew W. Skow, Air Force Wright Aeronautical Laboratories, and Eidetics Incorporated (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Development of procedures for large scale automated minimum weight structural design (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by Ronald A. Gellatly and Bell Aerospace Textron (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Development of procedures for large scale automated minimum weight structural design (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1968), also by Ronald A. Gellatly, John A. Bruno, and Bell Aerospace Textron (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Development of weapon delivery models and analysis programs. Volume I, System modeling and performance optimization (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by A. Ferit Konar, Honeywell Inc. Systems and Research Division, and Armament Delivery Analysis Programming System (ADAPS) (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Development of weapon delivery models and analysis programs. Volume II, Documentation of the Armament Delivery Analysis Programming System (ADAPS) (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by A. Ferit Konar, Michael D. Ward, Honeywell Inc. Systems and Research Division, and Armament Delivery Analysis Programming System (ADAPS) (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Development of weapon delivery models and analysis programs. Volume III, Testing and demonstration of the Armament Delivery Analysis Programming System (ADAPS) (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by A. Ferit Konar, Michael D. Ward, Honeywell Inc. Systems and Research Division, and Armament Delivery Analysis Programming System (ADAPS) (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Developments in structural analysis and synthesis by function minimization (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by Lucien A. Schmit and Case Western Reserve University (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Digital computer program for the analysis of crack propagation in cyclic loaded structures (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by R. G. Forman and J. P. Hudson (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Digital load control applied to full-scale airframe fatigue tests (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by Nirmal K. Mondol, Richard M. Potter, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Digital simulation of a Gaussian random process having an exponential autocorrelation function (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by D. K. Bowser and G. R. Schubert (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Directional thermal conductivities of graphite/epoxy composites: 0/90 and 0/ ± 45/90 (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), also by Lit S. Han, Leilani Glower, Air Force Wright Aeronautical Laboratories, and Ohio State University. Department of Mechanical Engineering (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Drag and dynamics of single and clustered parachutes in freestream, and with wake and ground effects (Wright-Patterson Air Force Base, Ohio, Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by Helmut G. Heinrich, R. A. Noreen, and University of Minnesota (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Drag and stability of cross type parachutes (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by R. J. Niccum, Robert Gutenkauf, E. L. Haak, United States. Air Force. Systems Command, and University of Minnesota. Department of Aerospace Engineering and Mechanics (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Drag measurements of upswept afterbodies and analytical study on axisymmetric separation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), also by Mansop Hahn, Theodore C. Nark, Paul E. Rubbert, Gunter W. Brune, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Durability methods development. Volume 1, Phase 1 summary (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by S. D. Manning, J. N. Yang, Masanobu Shinozuka, B. G. W. Yee, J. W. Norris, V. D. Smith, S. P. Henslee, S. M. Speaker, W. R. Garver, B. J. Pendley, and General Dynamics Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Durability methods development. Volume 2, Durability analysis: state-of-the-art assessment (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by S. D. Manning, Y. N. Kim, W. R. Garver, M. A. Flanders, and General Dynamics Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Durability methods development. Volume 3, Structural durability survey: state-of-the-art assessment (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by B. J. Pendley, S. D. Manning, S. P. Henslee, and General Dynamics Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Durability methods development. Volume 4, Initial quality representation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by Masanobu Shinozuka and Modern Analysis Inc (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Durability methods development. Volume 5, Durability analysis methodology development (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by J. N. Yang, W. R. Garver, S. D. Manning, General Dynamics Corporation, and George Washington University (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Dynamic response of shells to externally-applied dynamic loads (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by John W. Leech, Walter Herrmann, Emmett A. Witmer, Theodore H. H. Pian, United States. Air Force. Systems Command. Aeronautical Systems Division, and Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Dynamic stability of a parachute point-mass load system (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by H. G. Heinrich, L. W. Rust, United States. Air Force. Systems Command. Research and Technology Division, and University of Minnesota. Department of Aerospace Engineering and Mechanics (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Dynamic stability of a system consisting of a stable parachute and an unstable load (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by H. G. Heinrich, L. W. Rust, United States. Air Force. Systems Command. Research and Technology Division, and University of Minnesota (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Effect of fiber orientation on initial postbuckling behavior and imperfection sensitivity of composite cylindrical shells (Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970), also by N. S. Khot and V. B. Venkayya (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Effect of service environment on F-15 boron/epoxy stabilator (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by T. V. Hinkle, United States. Air Force. Systems Command, and McDonnell Douglas Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Effect of suction on the wake structure of a three-dimensional turret (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983, 1983), also by S. C. Purohit, Air Force Wright Aeronautical Laboratories, and University of Dayton. Research Institute (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The effect of surface perturbations on the pressure distributions about blunt two-dimensional bodies at high Mach numbers (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by Coleman duP. Donaldson, Wallace D. Hayes, Roger D. Sullivan, United States. Air Force. Systems Command, and Aeronautical Research Associates of Princeton (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Effects of combined acoustic and flight loads on crack growth (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1976., 1976), also by J. Soovere, S. T. Chiu, United States. Air Force. Systems Command, and Lockheed-California Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The effects of design parameters and local flow fields on the performance of hyperflo supersonic parachutes and high dynamic pressure parachute concepts (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by Leland W. Sims (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Effects of fighter attack spectrum on composite fatigue life (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by R. Badaliance, H. D. Dill, Air Force Wright Aeronautical Laboratories, and McDonnell Aircraft Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Effects of gust velocity spatial distributions on lateral-directional response of a VTOL aircraft (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Directorate of Laboratories, Air Force Systems Command, 1967., 1967), also by Robert L. Swaim and Alonzo J. Connors (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Effects of manipulator restraints on human operator performance (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by R. E. Magdaleno, Duane T. McRuer, Wright-Patterson Air Force Base (Ohio), Pa.). Laboratories for Research and Development Franklin Institute (Philadelphia, and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The effects of slip character and crack closure on the growth of small fatigue cracks in titanium-aluminium alloys (Wright-Patterson Air Force Base, Ohio : Materials Laboratory, Wright Research Development Center, Air Force Systems Command, Feb. 1990., 1990), also by James M. Larsen, Wright Research Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Effects of underloads on fatigue crack growth. Volume I, Technical summary (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by W. M. McGee, T. M. Hsu, United States. Air Force. Systems Command, and Lockheed-Georgia Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Effects of underloads on fatigue crack growth. Volume II, Data tabulations (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by W. M. McGee, T. M. Hsu, United States. Air Force. Systems Command, and Lockheed-Georgia Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Effects of variations in coldworking repair procedures on flaw growth and structural life (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984., 1984), also by J. M. Pearson-Smith, J. M. Potter, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Efficient ADI and spline ADI methods for the Navier-Stokes equations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), also by Michele Napolitano, Air Force Wright Aeronautical Laboratories, and University of Dayton. Research Institute (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Elasto-plastic analysis of structures under load and two-dimensional temperature distributions. Volume 1, Analysis development and experimental program (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by P. C. Huang, R. J. Edwards, United States. Air Force. Systems Command. Aeronautical Systems Division, and Martin Marietta Corporation. Baltimore Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Elasto-plastic analysis of structures under load and two-dimensional temperature distributions. Volume 2, Summary of test data (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by P. C. Huang, R. J. Edwards, United States. Air Force. Systems Command. Aeronautical Systems Division, and Martin Marietta Corporation. Baltimore Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Elasto-plastic analysis of structures under load and two-dimensional temperature distributions. Volume 3, Experimental evaluation of the general time-dependent analysis (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by R. J. Edwards, United States. Air Force. Systems Command. Aeronautical Systems Division, and Martin Marietta Corporation. Baltimore Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Elements of simulation error analysis (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by Richard F. Whitbeck, Air Force Wright Aeronautical Laboratories, and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Energy conversion systems reference handbook. Volume 9. Solar system design (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Flight Accessories Laboratory, Air Research and Development Command, United States Air Force, 1960., 1960), also by W. R. Menetrey, Electro-Optical Systems (Firm), United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Energy conversion systems reference handbook. Volume I. General systems condiserations (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Flight Accessories Laboratory, Air Research and Development Command, United States Air Force, 1960., 1960), also by W. R. Menetry, J. H. Fisher, Electro-Optical Systems (Firm), United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Energy conversion systems reference handbook. Volume III. Dynamic thermal converters (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Flight Accessories Laboratory, Air Research and Development Command, United States Air Force, 1960., 1960), also by C. W. Stephens, W. R. Menetry, R. Spies, Electro-Optical Systems (Firm), United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Energy conversion systems reference handbook. Volume V. Direct solar conversion (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Flight Accessories Laboratory, Air Research and Development Command, United States Air Force, 1960., 1960), also by W. Evans, W. R. Menetrey, Electro-Optical Systems (Firm), United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Energy conversion systems reference handbook. Volume VIII. Other devices (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Flight Accessories Laboratory, Air Research and Development Command, United States Air Force, 1960., 1960), also by R. Wall, D. McDowell, J. D. Burns, R. Spies, D. Erway, Electro-Optical Systems (Firm), United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Energy conversion systems reference handbook. Volume X. Reactor system design (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Flight Accessories Laboratory, Air Research and Development Command, United States Air Force, 1960., 1960), also by Electro-Optical Systems (Firm), United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Energy conversion systems reference handbook. Volume XI. Radioisotope system design (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Flight Accessories Laboratory, Air Research and Development Command, United States Air Force, 1960., 1960), also by Electro-Optical Systems (Firm), United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An Engineering evaluation of methods for the prediction of fatigue life in airframe structures (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, AIr Force Systems Command, United States Air Force, 1962., 1962), also by W. J. Crichlow, M. A. Melcon, L. Young, A. J. McCulloch, United States. Air Force. Systems Command. Aeronautical Systems Division, and Lockheed-California Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Enhanced ejection seat performance with vectored thrust capability (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), also by Lanny A. Jines, Edward O. Roberts, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Estimating times to early failures using sample data to estimate the Weibull scale parameter (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by Robert L. Neulieb and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Estimation of flying qualities of piloted airplanes (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems command, 1966., 1966), also by Robert J. Woodcock, D. E. Drake, Wright-Patterson Air Force Base (Ohio), and Douglas Aircraft Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Evaluation of a biaxial test fixture : interim report for period April 1981-October 1982 (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), also by James A. Holst and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Evaluation of a damage accumulation monitoring system as an individual aircraft tracking concept (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by C. L. Guadagnino, Air Force Wright Aeronautical Laboratories, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The evaluation of a digital hardware voter/monitor in an aircraft control system (Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1977), also by Harry W. Schreadley and inc Dynamic Controls (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Evaluation of separation criteria and their application to separated flow analysis (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory/FXM, Air Force Systems Command, 1973., 1973), also by Mansap Hahn, Avtar S. Mahal, Paul E. Rubbert, Boeing Commercial Airplane Company, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Evaluation of the NASA Electronic Strain-Level Counter as a Fatigue Damage Monitor (Wrigth-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by Larry E. Clay, Sandra K. Buehler, United States. Air Force. Systems Command, and Technology Incorporated (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Evaluation of the twin nozzle/afterbody drag and nozzle internal performance computer deck with ESIT free jet data (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, 1974., 1974), also by Phillip C. Everling and Douglas L. Bowers (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Evaluation of USSAERO and HABP computer codes for aerodynamic predictions for slender bodies (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by Jack I. Flaherty and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Evaluations of methods to predict flutter of wings with external stores (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), also by Sidney Siegel, Lowell V. Andrew, and North American Rockwell Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Experimental and analytical determination of integrated airframe nozzle performance. Volume I (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972, 1972), also by Edsel R. Glasgow, S. J. Smyth, R. F. Smith, D. K. Hill, R. D. Grennan, R. A. Fox, Leonard D. Miller, Don M. Santman, Lockheed-California Company, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Experimental and analytical determination of integrated airframe nozzle performance. Volume II, Operating manual for twin-nozzle/aftbody drag and internal nozzle performance computer deck (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by Edsel R. Glasgow, R. D. Grennan, R. A. Fox, Leonard D. Miller, Don M. Santman, Lockheed-California Company, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An experimental and analytical investigation of hypersonic inlet boundary layers (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by J. F. Stroud, L. D. Miller, and Lockheed-California Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Experimental and numerical analysis of axially compressed circular cylindrical fiber-reinforced panels with various boundary conditions (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by Nelson R. Bauld, Air Force Wright Aeronautical Laboratories, and Clemson University. Department of Mechanical Engineering (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Experimental and theoretical panel flutter studies in the mach number range of 1.0 to 5.0 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by E. H. Dowell, H. M. Voss, and Boeing Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Experimental and theoretical panel flutter studies in the mach number range of 1.0 to 5.0 : supplement 1 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by E. H. Dowell, United States. Air Force. Systems Command. Aeronautical Systems Division, and Boeing Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Experimental definition of top mounted inlet flow fields : Volume I (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by William W. Rhoades, Air Force Wright Aeronautical Laboratories, and Vought Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Experimental determination of the apparent moment of inertia of parachutes (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by Shukry K. Ibrahim, United States. Air Force. Systems Command, and University of Minnesota. Department of Aerospace Engineering and Mechanics (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Experimental investigation of pressures on a blunt two-dimensional profile and on sharp and blunt conical shapes of noncircular cross section at Mach 5 and 8 (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by Harold R. Mead, Frank Koch, United States. Air Force. Systems Command. Aeronautical Systems Division, Wright-Patterson Air Force Base (Ohio), and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An experimental investigation of shock wave -- boundary layer interaction dynamics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), also by Gerald W. Braun, William T. Snyder, and University of Tennessee (System). Space Institute (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Experimental investigation of the crack growth gage (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by Donald R. Holloway and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Experimental modal analysis and dynamic component synthesis (Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1987), also by Randall J Allemang and David L Brown (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Experimental studies of high temperature hypersonic diffusers (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by Richard T. Smith and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Experimental studies of the unstedy aerodynamics of panels at or near flutter with a finite boundary layer Mach number 1 to 10 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by G. W. Asher, A. W. Brown, United States. Air Force. Systems Command, and Boeing Aerospace Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An Experimental study of sharp and blunt 6 degree cones at large incidence with a turbulent boundary layer at Mach 6 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, High Speed Aero Performance Branch, Flight Mechanics Division, Air Force Systems Command, United States Air Force, 1974., 1974), also by E. D. McElderry, United States. Air Force. Systems Command, and Arnold Engineering Development Center (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An experimental study of the distribution of convective heat transfer to a large-scale model of parachute cloth (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by E. R. G. Eckert, K. M. Krall, C. J. Scott, M. Ruiz-Urbieta, J. E. Anderson, Wright-Patterson Air Force Base (Ohio), and University of Minnesota (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An experimental study on multi-wall structures for space vehicles (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Flight Dynamics Laboratory, Air Research and Development Command, U.S. Air Force, 1961., 1961), also by D. G. Younger, S. Lampert, Aeronutronic Ford Corporation, United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Experimental verification of the analyses and computer programs concerning heat transfer through semitransparent materials (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by H. Finch, C. Moeller, M. Noland, and Mo.) Midwest Research Institute (Kansas City (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Experiments on the thermal performance of ribbon parachutes (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by C. J. Scott, E. R. G. Eckert, United States. Air Force. Systems Command. Research and Technology Division, and University of Minnesota. Department of Mechanical Engineering (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Experiments to develop a thick turbulent boundary layer for optical degradation measurements (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Director of Laboratories, Air Force Systems Command, 1975., 1975), also by James T. Van Kuren (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Extended study of flaw growth at fastener holes. Volume 1 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1978., 1978), also by T. M. Hsu, J. A. Aberson, W. M. McGee, United States. Air Force. Systems Command, and Lockheed-Georgia Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Extended study of flaw growth at fastener holes. Volume 2, Data tabulation (Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1978), also by T. M. Hsu, W. M. McGee, United States. Air Force. Systems Command, and Lockheed-Georgia Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Extensions to the STAGS computer code (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by Bo O. Almroth, P. Stern, H. T. Petersen, E. Meller, F. A. Brogan, Lockheed Palo Alto Research Laboratory, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): F-4 Service Life Tracking Program (Crack Growth Gages) (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by Charles R. Saff, Air Force Wright Aeronautical Laboratories, and McDonnell Douglas Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Factors influencing the accuracy of aerodynamic hinge-moment prediction (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1978., 1978), also by Wen-Fan Lin, Michael D. Clarke, United States. Air Force. Systems Command, and Boeing Aerospace Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Fatigue/impact studies in laminated composites (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), also by V. Sarma Avva, Air Force Wright Aeronautical Laboratories, and North Carolina Agricultural and Technical State University (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Film cooling heat transfer with high free stream turbulence (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1996., 1996), also by John J. Schauer, David J. Pestian, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Finite deflection, discrete element analysis of shells (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by Fred K. Bogner and Case Western Reserve University (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Finite element analysis of transonic flow (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), also by S. T. K. Chan, M. R. Brashears, and Huntsville Research & Engineering Center (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Finite element modeling and optimization of aerospace structures (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by Walter J. Dwyer, Grumman Aerospace Corporation, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Finite element thermal-structural analysis of cable-stiffened space structures (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984., 1984), also by Earl A. Thornton, Ajay K. Pandey, Pramote Dechaumphai, Air Force Wright Aeronautical Laboratories, and Old Dominion University. Department of Mechanical Engineering and Mechanics (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Finite span effects on flap heating and effectiveness in a turbulent boundary layer (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by L. A. Cassel, S. Taylor, L. D. McMillen, Air Force Wright Aeronautical Laboratories, and inc Science Applications (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Fixed-base simulator investigation of the effects of L [alpha] and true speed on pilot opinion of longitudinal flying qualities (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1963., 1963), also by Charles R. Chalk and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Flat panel aircraft video LED display technology program. (Flight Dynamics Laboratory, Air Force Wright Aeornautical Laboratories, Air Force Systems Command, 1985), also by Optotek Limited (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Flat-plate boundary-layer transition at hypersonic speeds (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by R. E. Deem, J. S. Murphy, C. R. Erickson, North American Aviation, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Flaw growth in complex structure. Volume 1, Technical discussion (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1977., 1977), also by Thomas R. Brussat, M. Creager, S. T. Chiu, United States. Air Force. Systems Command, Del West Engineering, and Lockheed-California Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Flaw growth in complex structure. Volume 2, Test data (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1977., 1977), also by Thomas R. Brussat, M. Creager, S. T. Chiu, United States. Air Force. Systems Command, Del West Engineering, and Lockheed-California Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Flaw growth in complex structure. Volume 3, Summary, assessments, conclusions (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1977., 1977), also by Thomas R. Brussat, M. Creager, S. T. Chiu, United States. Air Force. Systems Command, Del West Engineering, and Lockheed-California Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Flexible plates and shells; a translation of [Gibkie plastinki i obolochki] (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by A. S. Volʹmir and University of Florida. Department of Engineering Sciences (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Flight control principles for control configured vehicles (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by Edmund G. Rynaski, Norman C. Weingarten, United States. Air Force. Systems Command, and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Flight evaluation of various short period dynamics at four drag configurations for the landing approach task (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by Charles R. Chalk, United States. Air Force. Systems Command, and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Flight investigation of fighter side-stick force-deflection characteristics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1975., 1975), also by G. Warren Hall and Rogers E. Smith (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A flight investigation of lateral-directional handling qualities for V/STOL aircraft in low speed maneuvering flight (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), also by K. H. Doetsch, D. M. McGregor, D. G. Gould, and National Aeronautical Establishment (Canada) (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Flight propulsion control coupling for thrust vectoring fighter aircraft. Volume III, Phase II (Wright-Patterson Air Force Base : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1980., 1980), also by Frederick C. Glaser and Douglas Aircraft Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Flight test evaluation of a digital multimode flight control system for the A-7D aircraft. Volume I, Design, analysis and ground test phase (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1975., 1975), also by Marv Bender, Knute Wefald, Larry Palker, Duane Oelschlaeger, Russell Hendrick, Robert Gaabo, George Cole, Air Force Wright Aeronautical Laboratories, and Honeywell Inc. Government and Aeronautical Products Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Flight test of advanced digital control concepts (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by Richard F. Whitbeck, Thomas T. Myers, James C. Smith, Air Force Wright Aeronautical Laboratories, and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Flight test results of a powered parafoil system (AeroFlyer) (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1976., 1976), also by John D. Nicolaides and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Flight text investigation of transonic shock-boundary layer phenomena (Wright-Patterson Air Force Base, Ohio : Air Force Systems Command, Air Force Flight Dynamics Laboratory, 1968., 1968), also by Jones F. Cahill, Bill L. Copper, and Lockheed-Georgia Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Force method optimization II. Volume I, Theoretical development (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by Batt J. R., R. A. Gellatly, S. Gellin, Air Force Wright Aeronautical Laboratories, and Bell Aerospace Textron (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Force method optimization II. Volume II, User's manual (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by Batt J. R., S. Gellin, D. L. Witkop, S. C. Skalski, B. J. Dale, Air Force Wright Aeronautical Laboratories, and Bell Aerospace Textron (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): FORMAT : Fortran matrix abstraction technique. Volume 5, Supplement II. Engineering user and technical report-extended (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1973., 1973), also by John Pickard, Air Force Wright Aeronautical Laboratories, and Douglas Aircraft Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): FORMAT : Fortran matrix abstraction technique. Volume 6. Description of digital computer program - Phase 1 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by J. P. Cogan, J. R. Wells, J. E. Serpanos, R. C. Morris, Air Force Wright Aeronautical Laboratories, and Douglas Aircraft Company. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): FORMAT : Fortran matrix abstraction technique. Volume 6 - Supplement 2. Description of digital computer program - Phase 1 - Extended (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by R. C. Morris, Air Force Wright Aeronautical Laboratories, and Douglas Aircraft Company. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): FORMAT : Fortran matrix abstraction technique. Volume 7 - Supplement 1. Description of digital computer program - Phase 3 - Extended (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by J. A. Frank, Air Force Wright Aeronautical Laboratories, and Douglas Aircraft Company. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): FORMAT : Fortran matrix abstraction technique. Volume V. Engineering user and technical report (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1968., 1968), also by John Pickard, Air Force Wright Aeronautical Laboratories, and Douglas Aircraft Company. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): FORMAT : Fortran matrix abstraction technique. Volume V, Supplement I. Engineering user and technical report extended (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1970., 1970), also by John Pickard, Air Force Wright Aeronautical Laboratories, and Douglas Aircraft Company. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): FORMAT : Fortran matrix abstraction technique. Volume VII. Description of digital computer program - Phase 3 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by R. C. Morris, P. S. Yoon, J. R. Wells, Air Force Wright Aeronautical Laboratories, and Douglas Aircraft Company. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): FORMAT II - Second version of Fortran matrix abstraction technique. Volume 3, A User-coded matrix generator for the force method (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by R. C. Morris and Douglas Aircraft Company. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Forward swept wing static aeroelasticity (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by Terry A. Weisshaar, Air Force Wright Aeronautical Laboratories, and Virginia Polytechnic Institute and State University. Aerospace and Ocean Engineering Department (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Fracture control procedures for aircraft structural integrity (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by Howard A. Wood (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Fracture mechanics analysis of single and double rows of fastener holes loaded in bearing (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1976., 1976), also by Oscar Orringer and George Stalk (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Frequency domain design of robust controllers for space structures (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Research and Development Center, Air Force Systems Command, United States Air Force, 1989., 1989), also by William Howard Bennett, C. LaVigna, Wright Research and Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Further studies of multiple regression analysis of human pilot dynamic response: a comparison of analysis techniques and evaluation of time-varying measurements (Wright-Patterson Air Force Base, Ohio : Flight Control Division, Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by Jerome I. Elkind, Beranek Bolt, Wright-Patterson Air Force Base (Ohio), and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): General instability of orthotropically stiffened cylinders. Part 1, Axial compression, torsion and hydrostatic pressure loadings (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, AIr Force Systems Command, United States Air Force, 1965., 1965), also by Roger Milligan, Herbert Becker, C. Lakshmikantham, George Gerard, and Allied Research Associates (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): General instability of orthotropically stiffened cylinders. Part 2, Bending and combined compression and bending (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, AIr Force Systems Command, United States Air Force, 1965., 1965), also by C. Lakshmikantham, Roger Milligan, George Gerard, and Allied Research Associates (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Generalized procedures for tracking crack growth in fighter aircraft (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by G. S. Parker, United States. Air Force. Systems Command, and McDonnell Aircraft Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A graphic method for predicting audibility of noise sources (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by S. A. Fidell, Richard Horonjeff, Beranek Bolt, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Ground simulator evaluations of coupled roll-spiral mode effects on aircraft handling qualities (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by Frederick D. Newell and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A guide for predicting the vibrations of fighter aircraft in the preliminary design stages (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by Eric E. Ungar, Grumman Aerospace Corporation, and Beranek Bolt (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Handbook of force management methods (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by A. P. Berens, D. J. White, C. E. Larson, R. L. Johnson, J. C. Davis, K. E. Brown, D. S. Morcock, Air Force Wright Aeronautical Laboratories, Vought Corporation, Lockheed-Georgia Company, and University of Dayton. Research Institute (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Heat transfer measurements at Mach 8 on an aerodynamically controllable winged re-entry configuration : part of an investigation of hypersonic flow separation and control characteristics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by Lawrence Meckler, United States. Air Force. Systems Command, and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Heat transfer measurements in cold wind tunnels (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by H. L. Moody, K. Jechel, Air Force Wright Aeronautical Laboratories, and Calif.) PDA Engineering (Firm : Santa Ana (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Heating in regions of interfering flow fields (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by C. E. Gulbran, S. L. Strack, D. S. Miller, and E. Redeker (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Heavy equipment aerial delivery and retrieval techniques (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Div., Air Force Systems Command, 1967., 1967), also by Elwood L. White, R. F. Sturneon, and C. E. Bronn (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Hereditary models for airfoils in unsteady aerodynamics : numerical approximations and parameter estimation (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by J. A. Burns, E. M. Cliff, Air Force Wright Aeronautical Laboratories, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): HIgh acceleration cockpit controller locations (Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1975), also by McDonnell Aircraft Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): High altitude gust criteria for aircraft design (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), also by Edward V. Ashburn, Craig A. Melvin, David E. Waco, United States. Air Force. Systems Command, and Lockheed-California Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): High angle of attack missile aerodynamics at Mach numbers 0.30 to 1.5 (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by Valentine Dahlem, Christian E. G. Przirembel, Donald E. Shereda, Jack I. Flaherty, Air Force Wright Aeronautical Laboratories, and Rutgers University (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): High speed flight effects on noise propagation (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1986., 1986), also by R. H. Burrin, M. Salikuddin, K. K. Ahuja, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): High speed flow separation ahead of finite span steps (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1978., 1978), also by Louis G. Kaufman, Robert D. Kirchner, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): High-speed-performance analysis : nominal and optimal boost climb performance analysis (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1987., 1987), also by L. Earl Miller and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): High speed smoke flow visualization (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by Stephen M. Batill, T. J. Mueller, Robert C. Nelson, Air Force Wright Aeronautical Laboratories, and University of Notre Dame. Department of Aerospace and Mechanical Engineering (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): High vacuum measuring instrumentation and methodology. (Clearinghouse for Federal Scientific and Technical Information], 1964), also by Jonathan R. Roehrig and National Research Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Holographic investigation of slender body vortex wakes (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by F. D. Deffenbaugh, J. L. Jacoby, Air Force Wright Aeronautical Laboratories, and TRW Inc. Systems and Energy (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Horizontal shear testing of woven fiberglass/epoxy composites (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), also by Robert T. Achard and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Human pilot dynamic response in single-loop systems with compensatory and pursuit displays (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by R. J. Wasicko, R. E. Magdaleno, Duane T. McRuer, Wright-Patterson Air Force Base (Ohio), and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Human pilot dynamics with various manipulators (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by Duane T. McRuer, R. E. Magdaleno, Wright-Patterson Air Force Base (Ohio), and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Hybrid aerodynamic methods (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984., 1984), also by Frank A. Dvorak, Donald W. Roberts, Gerald C. Paynter, T. S. Vaidyanathan, James K. Nathman, Brian Maskew, Air Force Wright Aeronautical Laboratories, Boeing Military Airplane Company, and Inc Analytical Methods (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Hypersonic blunt body similitude in a perfect gas (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by G. M. Gregorek, K. D. Korkan, United States. Air Force. Systems Command, and Ohio State University (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Hypersonic boundary layer transition experiments (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by Kenneth F. Stetson and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Hypersonic boundary layer transition experiments. Part I. Nosetip bluntness effects on cone frustum transition. Part II. Mach 6 experiments of transition on a cone at angle of attack (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1986., 1986), also by Kenneth F. Stetson and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Hypersonic dynamic stability. Part I. Summary (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by L. A. Marshall and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Hypersonic dynamic stability Part II. Conical body experimental program (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by R. B. Hobbs, United States. Air Force. Systems Command, and General Electric Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Identification of dynamic structures with special attention to damping matrix representation (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate, Wright Laboratory, Air Force Systems Command, United States Air Force, 1992., 1992), also by Jay H. Kim and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Impact damage tolerance of composites exposed to hot, cold and wet environments (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Research and Development Center, Air Force Systems Command, United States Air Force, 1991., 1991), also by V. Sarma Avva, North Carolina Agricultural and Technical State University, Wright Research and Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Improved dynamic models for air combat analysis (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by N. Farber, J. Shinar, M. Negrin, Air Force Wright Aeronautical Laboratories, and Israel) Mosad ha-Ṭekhniyon le-meḥḳar u-fituaḥ (Haifa (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Improvements of finite element solutions for structural and nonstructural applications (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by G. Sander, F. de Veubeke, P. Beckers, Université de Liège. Laboratoire de Techniques Aéronautiques et Spatiales, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): In-flight investigation of the effects of higher-order control system dynamics on longitudinal handling qualities (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1968., 1968), also by Dante A. Di Franco, Cornell Aeronautical Laboratory, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Including fleet usage variability in reliability analyses for both safety and economic limit (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by Robert L. Neulieb and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Infinite mass operating case (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1966., 1966), also by H. D. Melzig, P. K. Schmidt, and Deutsche Forschungsanstalt für Luft- und Raumfahrt (1961-1969) (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Influence of forebody geometry on aerodynamic characteristics and a design guide for defining departure/spin resistant forebody configurations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Research and Development Center, Air Force Systems Command, United States Air Force, 1989., 1989), also by William Bihrle, E. Dickes, B. Barnhart, Inc Bihrle Applied Research, Wright Research and Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Influence of pitching moment characteristics on departure and uncoordinated roll reversal boundaries for fighter configurations (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force WRight Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by William. Jr Bihrle, B. Barnhart, Air Force Wright Aeronautical Laboratories, and Inc Bihrle Applied Research (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Influence of residual stresses and thermal gradients on mechanism of buckling of shallow spherical shells (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by Megumi Sunakawa, R. M. Evan-Iwanowski, and Syracuse University. Research Institute (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Inhibition of flow separation at high speed. Volume 1, Supersonic turbulent boundary layers (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), also by Larry L. Lynes, Frederick K. Goodwin, Jack Norman Nielsen, and Nielsen Engineering & Research (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Inhibition of flow separation at high speed. Volume 2, Calculation of nonadiabatic laminar boundary layers (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), also by Frederick K. Goodwin, Larry L. Lynes, Jack Norman Nielsen, and Nielsen Engineering & Research (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Inhibition of flow separation at high speed. Volume 3, Experimental results for laminar boundary layers (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), also by Jack Norman Nielsen, Frederick K. Goodwin, Larry L. Lynes, and Nielsen Engineering & Research (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Inhibition of flow separation at high speed. Volume IV, Calculation of nonadiabatic laminar boundary layers on conical compression surfaces (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), also by Frederick K. Goodwin, Larry L. Lynes, and Nielsen Engineering & Research (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Initial quality of advanced joining concepts (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984., 1984), also by W. R. Garver, K. M. Koepsel, D. Y. Lee, Air Force Wright Aeronautical Laboratories, and General Dynamics Corporation. Fort Worth Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Initial VTOL flight control design criteria development - discussion of selected handling qualities topics : first yearly report / John Kroll, Jr. (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by John. Jr Kroll and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Inspection periods determined from data of crack development and strength reduction of an aircraft structure using static analysis (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by Sigge Eggwertz, United States. Air Force. Systems Command. Aeronautical Systems Division, and Flygtekniska försöksanstalten (Sweden) (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Integrated airframe - nozzle performance for designing twin-engine fighters. Volume I (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by Edsel R. Glasgow, D. K. Hill, R. D. Grennan, R. A. Fox, Leonard D. Miller, Don M. Santman, and Lockheed-California Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Integrated airframe - nozzle performance for designing twin-engine fighters. Volume II, Wind tunnel data identification and presentation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by Edsel R. Glasgow, T. J. Jones, D. A. Tappeiner, T. E. Charbonneau, D. K. Hill, R. D. Grennan, R. A. Fox, D. A. Fox, Leonard D. Miller, Don M. Santman, and Lockheed-California Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Integrated airframe - nozzle performance for designing twin-engine fighters. Volume IV, Operating manual for subsonic axisymmetric nozzle boattail drag computer deck (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by Edsel R. Glasgow, T. J. Jones, T. E. Charbonneau, Leonard D. Miller, Don M. Santman, and Lockheed-California Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Integrated airframe - nozzle performance for designing twin-engine fighters. Volume V, Operating manual for supersonic axisymmetric nozzle boattail drag computer deck (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by Edsel R. Glasgow, T. J. Jones, T. E. Charbonneau, Leonard D. Miller, Don M. Santman, and Lockheed-California Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Integrated airframe - nozzle performance for designing twin-engine fighters. Volume VI, Revised operating manual for twin nozzle/afterbody drag and nozzle internal performance computer deck (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by Edsel R. Glasgow, D. A. Tappeiner, R. Posthumus, R. D. Grennan, R. A. Fox, Leonard D. Miller, Don M. Santman, and Lockheed-California Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Interactive composite joint design. Part 1, Final technical report (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1978., 1978), also by M. K. Smith, C. G. Dietz, L. J. Hart-Smith, United States. Air Force. Systems Command, and Douglas Aircraft Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Interactive composite joint design. Part 3, Programming manual (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1978., 1978), also by M. K. Smith, C. G. Dietz, L. J. Hart-Smith, United States. Air Force. Systems Command, and Douglas Aircraft Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Interactive graphics program for computing three-degree-of-freedom store separation trajectories at speeds up to the critical speed (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Flight Control Division, Control Criteria Branch, Air Force Systems Command, United States Air Force, 1972., 1972), also by Calvin L. Dyer and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Introduction to computational aerodynamics (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), also by W. L. Hankey and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Investigation of ablation effects on hypersonic dynamic stability of a 10 cone (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by Dave R. Moore, Thomas C. Pope, Charles J. Stalmach, and LTV Aerospace Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An investigation of an integrated aircrew escape/rescue capability (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Vehicl Equipment Division, Air Force Systems Command, United States Air Force, 1969., 1969), also by R. J. Manzuk, J. W. Olcott, Edward Seckel, L. A. Pond, James W. Duncan, Walter R. Peck, N. J. Bentzen, E. A. Braunlich, and Charles A. Yost (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Investigation of cross wind effects on stable parachute point-mass systems (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by Helmut G. Heinrich, T. C. Nietz, Wright-Patterson Air Force Base (Ohio), and University of Minnesota (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Investigation of drag reduction by boundary-layer suction on a body of revolution at Mach numbers 2.5, 3, and 3.5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Kármán Gas Dynamics Facility, Air Research and Development Command, United States Air Force, 1965., 1965), also by S. R. Pate, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Investigation of flying qualities of military aircraft at high angles of attack. Volume I, Technical results (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), also by Donald E. Johnston, Jeffrey R. Hogge, Irving L. Ashkenas, and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Investigation of flying qualities of military aircraft at high angles of attack. Volume II, Appendices (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), also by Donald E. Johnston, Gary L. Teper, Jeffrey R. Hogge, and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Investigation of high-AOA flying qualities : criteria and design guides (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by Donald D. Johnston, Robert K. Heffley, Air Force Wright Aeronautical Laboratories, and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): An investigation of hypersonic flow separation and control characteristics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by Louis G. Kaufman, Daniel Weiss, Stravos Hartofilis, Lawrence Meckler, United States. Air Force. Systems Command. Research and Technology Division, and Grumman Aircraft Engineering Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Investigation of hypersonic inlet shock-wave boundary layer interaction. Part I (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by Paul H Kutschenreuter, Paul H. Nettleton, James A. Weil, James S. Keith, United States. Air Force. Systems Command. Research and Technology Division, and General Electric Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Investigation of measuring system requirements for instrument low visibility approach (Wright-Patterson AFB, Ohio : Air Force Flight Dynamics Laboratory, Aeronautical Systems Division, United States Air Force, 1971., 1971), also by Dunstan Graham, Lee Gregor Hofmann, Warren F. Clement, United States. Air Force. Systems Command, and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Investigation of numerical techniques as applied to digital flight control systems (Wright-Patterson Air Force Base, Ohio, Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by J. W. Hung, J. A. Spicer, P. P. Shipley, K. W. Nielsen, C. L. Lutes, Wright-Patterson Air Force Base (Ohio), and North American Aviation. Autonetics Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Investigation of numerical techniques for predicting aerodynamic heating to flight vehicles (Wright-Patterson Air Force Base : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1979., 1979), also by Arthur B. Lewis and Neil J. Sliski (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Investigation of stabilization and control systems for application to aero space vehicle escape capsules (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by F. E. Chew, H. A. Clutz, L. Oling, United States. Air Force. Systems Command. Aeronautical Systems Division, and Chance Vought Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Investigation of stress-strain history modeling at stress risers : Phase 1 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by James R. Carroll, G. J. Gilbert, R. F. Wilkinson, United States. Air Force. Systems Command, and Lockheed-Georgia Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Investigation of stress-strain history modeling at stress risers : Phase 2 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1978., 1978), also by James R. Carroll, R. F. Wilkinson, R. L. Brugh, and Lockheed-Georgia Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Investigation of subsonic duct distortion (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), also by C. J. MacMiller and North American Rockwell Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Investigation of the effects of gusts on V/STOL craft in transition and hover (Wright-Patterson Air Force Base : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by Grant Brandford Skelton and Honeywell Inc. Systems and Research Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Investigation of the flow field during the inflation of clustered parachutes (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by R. J. Niccum, Nebojsa D. Kovacevic, and University of Minnesota (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Investigation of the thermal properties of high-temperature insulation materials (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by A. E. Wechsler, Peter E. Glaser, United States. Air Force. Systems Command. Aeronautical Systems Division, Inc Arthur D. Little, Wright-Patterson Air Force Base (Ohio), and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A Kinetic theory development of the equations of motion of a diatomic gas (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1986., 1986), also by William Z. Strang and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A Koiter-type method for finite element analysis of nonlinear structural behavior. Volume 1, The Modified Structure method (Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970), also by Raphael T. Haftka, W. Nachbar, R. H. Mallett, and San Diego University of California (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A Koiter-type method for finite element analysis of nonlinear structural behavior. Volume 2, User's manual for program BEHAVE (Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970), also by Raphael T. Haftka, W. Nachbar, R. H. Mallett, and San Diego University of California (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A laboratory investigation into flight path perturbations during steep descents of V/STOL aircraft (Wright-Patterson AFB, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1976), also by L. D. Reid, Peter C. Hughes, H. W. Teunissen, Bernard Etkin, United States. Air Force. Systems Command, and University of Toronto. Institute for Aerospace Studies (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Laminar boundary layer along inviscid surface streamlines over inclined axisymmetric bodies in incompressible flow (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1988., 1988), also by Fred R. DeJarnette, Lee H. Kania, Air Force Wright Aeronautical Laboratories, and North Carolina State University. Department of Mechanical and Aerospace Engineering (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Laminate tubular specimens subjected to biaxial stress states. Volume II, Graphite/Epoxy (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1975., 1975), also by R. S. Sandhu, J. E. Pappas, M. D. Richardson, E. E. Zink, F. E. Hussong, J. B. Monfort, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Large amplitude response of complex structures due to high intensity noise (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by C. Mei and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Large deflection and stability analysis of two-dimensional truss and frame structures (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by J. S. Przemieniecki, D. M. Purdy, and Air Force Institute of Technology (U.S.) (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Lateral-directional oscillatory handling qualities (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by I. L. Ashkenas, Wright-Patterson Air Force Base (Ohio), and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Low Altitude Atmospheric Turbulence LO-LOCAT phase III interim report. Volume I, Data acquisition and analysis (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), also by K. R. Monson, R. H. Mielke, G. W. Jones, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Low-density flow effects for hypervelocity vehicles : phase II (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Research Development Center, United States Air Force Systems Command, 1990., 1990), also by Roop N. Gupta, Sudheer N. Nayani, Inc ViGYAN, Wright Research and Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Low density real gas flows about hypersonic vehicles (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1988., 1988), also by J. J. Hoffman, S. F. Birch, R. R. Bussing, R. S. Wong, Air Force Wright Aeronautical Laboratories, and Boeing Aerospace Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Low frequency instabilities of free systems (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by Robert G. Schwendler, Jack H. Hill, Computer Engineering Associates, Wright-Patterson Air Force Base (Ohio), and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Low Reynold number turbine blade cascade calculations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1996., 1996), also by Richard Byram Rivir, Elizabeth Ervin, Michael Dahlstom, Rolf Sondergaard, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Low speed aerodynamics for ultra-quiet flight (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by R. A. Kroeger, T. C. Helvey, H.D. Gruschka, and University of Tennessee (System). Space Institute (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Low-speed investigations of 'Apex Fence' and 'Cavity Flap' concepts on a 60 degree delta configuration (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1987., 1987), also by Dhanvada M. Rao, Charles T. L. Mills, Keith D. Hoffler, Air Force Wright Aeronautical Laboratories, and Vigyan Research Associates (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Mach 0.6 to 3.0 flows over rectangular cavities (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), also by Louis G. Kaufman, Rodney L. Clark, Algirdas Maciulaitis, Air Force Wright Aeronautical Laboratories, and Grumman Aerospace Corporation. Research and Development Center (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): MAGIC : an automated general purpose system for structural analysis. Volume 2, User's manual (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), also by Stephen Jordan, Bell Aerospace Textron, Robert H. Mallett, and Gene E. Maddux (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): MAGIC : n automated general purpose system for structural analysis. Volume 1, Engineer's manual (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), also by Robert H. Mallett, Stephen Jordan, and Bell Aerospace Textron (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The Mark IV Supersonic-Hypersonic Arbitrary-body Program. Volume I, User's manual (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by Arvel E. Gentry, Wayne R. Oliver, Douglas N. Smyth, and Douglas Aircraft Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The Mark IV Supersonic-Hypersonic Arbitrary-body Program. Volume II, Program formulation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by Arvel E. Gentry, Wayne R. Oliver, Douglas N. Smyth, and Douglas Aircraft Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Mark IV supersonic-hypsersonic arbitrary-body program modifications and computer graphics. Volume I, Surface streamline tracing (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by S. Taylor, Air Force Wright Aeronautical Laboratories, and inc Science Applications (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Mark IV supersonic-hypsersonic arbitrary-body program modifications and computer graphics. Volume II, Computer graphics (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by S. Taylor, Air Force Wright Aeronautical Laboratories, and inc Science Applications (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Mass injection and jet flow simulation effects on transonic afterbody drag (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1978., 1978), also by Wladimiro Calarese, Ronald E. Walterick, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Mathematical analysis of heat conduction in a sector of a hollow circular cylinder (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by Martin Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Matrix analysis methods for anisotropic inelastic structures (Wright-Patterson Air Force Base, Ohio: Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by W. R. Jensen, N. Prince, W. E. Falby, and Grumman Aircraft Engineering Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Matrix analysis of shells : small and large displacements (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by J. H. Argyris, P. C. Patton, K. E. Buck, W. Bosshard, and J. B. Spooner (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Matrix-dominated time-dependent deformation and damage of graphite epoxy composite experimental data under ramp loading (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by Edward M. Wu, Nhan Q. Nguyen, Richard L Moore, Air Force Wright Aeronautical Laboratories, and Lawrence Livermore National Laboratory (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Matrix-dominated time-dependent deformation and damage of graphite-epoxy composite : experimental data under multiple-step relaxation (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Forc, 1983., 1983), also by Edward Ming-chi Wu, Richard L. Moore, Nhan Q. Nguyen, Air Force Wright Aeronautical Laboratories, and Lawrence Livermore National Laboratory (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Matrix methods in structural mechanics 1965- (Wright-Patterson Air Force Base], 1965), also by Conference on Matrix Methods in Structural Mechanics (Wright-Patterson Air Force Base), United States. Air Force. Systems Command, and Air University United States. Air Force. Institute of Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The measurement of crack tip stresses by X-ray diffraction (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1978., 1978), also by John E. Allison and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The measurement of velocity and temperature in a hypersonic laminar boundary layer (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by John D. Lee, Ohio State University. Aeronautical and Astronautical Research Laboratory, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Medium altitude critical atmospheric turbulence (MEDCAT) data processing and analysis (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by J. P. Ryan, Kurt C. Rolle, Robert J. Dominic, A. C. Robertson, A. P. Berens, and University of Dayton. Research Institute (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A method for assessing the impact of wake vortices of USAF operations (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories. Air Force Systems Command, United States Air Force, 1979., 1979), also by George Kurylowich and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A method for calculating helicopter vortex paths and wake velocities (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), also by E. S. Levinsky, T. Strand, Air Vehicle Corporation, and Wright-Patterson Air Force Base (Ohio) (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A method for predicting thermal response in sandwich panels (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by P. J. Kendall, T. E. Chappell, J. P. Moran, United States. Air Force. Systems Command. Aeronautical Systems Division, and Martin Marietta Aerospace (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A method for predicting three-degree-of-freedom store separation trajectories at speeds up to the critical speed (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1974., 1974), also by Frederick K. Goodwin, Marnix F. E. Dillenius, Jack Norman Nielsen, and Nielsen Engineering & Research (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The method of characteristics for three-dimensional real-gas flows : including the digital computer program details and operating procedures for frozen flows (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by Charles R. Strom and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Method of determining reduction in elevator effectiveness when engine is mounted on aft fuselage of aircraft (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by James R. Atchison, United States. Air Force. Systems Command, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Methodologies for the direct digital control of highly flexible vehicles (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), also by Duane T. McRuer, Raymond E. Magdaleno, Richard F. Whitbeck, Air Force Wright Aeronautical Laboratories, and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Methods for predicting the aerodynamic and stability and control characteristics of STOL aircraft. Volume II, STOL aerodynamic methods computer program (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by M. I. Goldhammer, N. F. Wasson, and Douglas Aircraft Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Methods for predicting the aerodynamic and stability and control characteristics of STOL aircraft. Volume III, Engineering methods (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by M. I. Goldhammer, M. L. Lopez, and Douglas Aircraft Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Missile Datcom. Volume I, Final report (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1988., 1988), also by Steven R. Vukelich, Marvin Moore, Joseph A. Castillo, Keith A. Burns, Stan Stoy, Air Force Wright Aeronautical Laboratories, and McDonnell Douglas Astronautics Company-St. Louis (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Missile Datcom. Volume II, User's manual (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1988., 1988), also by Steven R. Vukelich, Marvin Moore, Stan Stoy, Air Force Wright Aeronautical Laboratories, and McDonnell Douglas Astronautics Company-St. Louis (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Missile supersonic/hypersonic aerodynamics (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate, Wright Laboratory, Air Force Systems Command, United States Air Force, 1991., 1991), also by Andrew A. Jenn, Philip K. Wang, Carol D. Matthews, McDonnell Douglas Astronautics Company-St. Louis, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Modal control of structural systems (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984., 1984), also by D. F Miller, W. R. Wells, Air Force Wright Aeronautical Laboratories, and Wright State University (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Modal investigation of lightweight aircraft structures using digital techniques (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by Robert W. Gordon, Richard D. Talmadge, H. F. Wolfe, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Modeling flexible aircraft for flight control design (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1989., 1989), also by E. C. Bekir, G. A. Watts, R. N. Moon, E. J. Horowitz, H. Hassig, A. Goforth, William Davis, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Modeling, identification and control of flexible aircraft (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984., 1984), also by Horst Salzwedel, James H. Vincent, Air Force Wright Aeronautical Laboratories, and Inc Systems Control Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Multifunction flight control reference system. Volume 1, Design and development (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by Gene E. Barnard, Sven P. Greenquist, John F. Susek, William J. Luedde, David L. Sebring, Air Force Wright Aeronautical Laboratories, and McDonnell Aircraft Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Multivariable flight control design with uncertain parameters (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by Isac Horowitz, B. Golubev, L. Neumann, Oded Yaniv, Z. Kopelman, Air Force Wright Aeronautical Laboratories, University of Colorado Boulder. Department of Electrical Engineering, and Mekhon Ṿaitsman le-madaʻ (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Multivariable methods for the design, identification, and control of large space structures. Volume 1, Estimator eigenvalue placement in positive real design (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Research and Development Center, Air Force Systems Command, United States Air Force, 1989., 1989), also by Gary Lewis Slater, M. D. McLaren, University of Cincinnati. Department of Aerospace Engineering and Engineering Mechanics, Wright Research and Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Multivariable methods for the design, identification, and control of large space structures. Volume 1, Optimal and sub-optimal estimation applied to large flexible structures (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Research and Development Center, Air Force Systems Command, United States Air Force, 1989., 1989), also by S. Dumbacher, University of Cincinnati. Department of Aerospace Engineering and Engineering Mechanics, Wright Research and Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): NASTRAN stress recovery package (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by Steven E. Lamberson and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): New approaches to flight vehicle structural vibration analysis and control (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by Manfred A. Heckl, Eric E. Ungar, G. Maidanik, Richard H. Lyon, United States. Air Force. Systems Command. Aeronautical Systems Division, and Beranek Bolt (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): New approaches to human-pilot/vehicle dynamic analysis (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by Duane T. McRuer, Julian Wolkovitch, D. H. Weir, Anil V. Phatak, G. P. Moore, Henry R. Jex, L. G. Hofmann, and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Noise and sonic fatigue of high lift devices. aeroacoustic loads (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by H. L. Leve, D. A. Plocher, C. M. Ho, M. A. Yeneriz, United States. Air Force. Systems Command, University of Southern California, and Douglas Aircraft Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A non-gaussian turbulence simulation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), also by Paul M. Reeves (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A Nonarbitarary fatigue crack size concept to predict total fatigue lives (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by Peter Kurath, JoDean Morrow, D. F. Socie, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Nonlinear and thermal effects on elastic vibrations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by Raymond C. Weikel, Bruce E. Greene, Harold C. Martin, James A. Seiler, Robert E. Jones, Boeing Company, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Nonlinear flying quality parameters based on dynamic inversion (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1987., 1987), also by B. G. Morton, G. Hines, C. A. Harvey, Michael Ray Elgersma, Air Force Wright Aeronautical Laboratories, and Honeywell Systems and Research Center (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Nonlinear thermoelastic effects on hypersonic stability and control. Part 1, Volume 1. Aerodynamics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by James R. Batt, United States. Air Force. Systems Command, Wright-Patterson Air Force Base. Flight Dynamics Laboratory, and Bell Aircraft Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Nonlinear thermoelastic effects on hypersonic stability and control. Part 1, Volume 2 : Aerodynamics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by James R. Batt, United States. Air Force. Systems Command, and Bell Aircraft Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Nonlinear thermoelastic effects on hypersonic stability and control. Part II. Analytical and experimental static aerothermoelasticity (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by James R. Batt, Richard H. Gallagher, United States. Air Force. Systems Command, Wright-Patterson Air Force Base. Flight Dynamics Laboratory, and Bell Aircraft Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Nonlinear thermoelastic effects on hypersonic stability and control. Part III. Simulation, measurement and analysis of nonlinear static aerothermoelastic behavior of a 45 degrees delta wing (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by James R. Batt, United States. Air Force. Systems Command, and Wright-Patterson Air Force Base. Flight Dynamics Laboratory (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Numerical aircraft design using 3-D transonic analysis with optimization. Volume 1, Executive summary (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by Andrew J. Srokowski, P. Aidala, M. E. Lores, Air Force Wright Aeronautical Laboratories, Grumman Aerospace Corporation, and Lockheed-Georgia Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Numerical aircraft design using 3-D transonic analysis with optimization. Volume 2 Part 1, Fighter design (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by P. Aidala, Air Force Wright Aeronautical Laboratories, Grumman Aerospace Corporation, and Lockheed-Georgia Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Numerical aircraft design using 3-D transonic analysis with optimization. Volume 2 Part 1, Transport design (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by Andrew J. Srokowski, P. R. Simth, R. A. Weed, M. E. Lores, Air Force Wright Aeronautical Laboratories, Grumman Aerospace Corporation, and Lockheed-Georgia Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Numerical aircraft design using 3-D transonic analysis with optimization. Volume 3 Part 1, User's guide to transport design computer programs (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by R. A. Weed, Andrew J. Srokowski, Air Force Wright Aeronautical Laboratories, Grumman Aerospace Corporation, and Lockheed-Georgia Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Numerical methods for imperfection sensitivity analysis of stiffened cylindrical shells. Volume 1. Development and applications (Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1986), also by Richard L. Citerley, Narendra S. Khot, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Numerical simulation of flow around a three-dimensional turret (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by S. C. Purohit and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Numerical solutions for steady and unsteady oscillatory flow about an axi-symmetric inlet (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983, 1983), also by Richard W. Newsome and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): On design of off-axis specimens (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), also by Raghbir Singh Sandhu, George Peter Sendeckyj, Air Force Wright Aeronautical Laboratories, and Inc Analytical Methods (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): On the effects of fiber orientation and nonhomogeneity on buckling and postbuckling equilibrium behavior of fiber-reinforced cylindrical shells under uniform axial compression (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by N. S. Khot (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): On Vortex breakdown and instability (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by S. N. Singh, Wilbur L. Hankey, Air Force Wright Aeronautical Laboratories, and Southeastern Center for Electrical Engineering Education (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Operational utility survey: supermaneuverability (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984., 1984), also by William L. Hamilton, Andrew M. Skow, Air Force Wright Aeronautical Laboratories, and Eidetics Incorporated (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): OPTIM III : a NASTRAN compatible large scale automated minimum weight design problem-users and programmers manual (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by B. J. Dale, R. D. Thom, J. Padlog, Air Force Wright Aeronautical Laboratories, and Bell Aerospace Textron (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Optimal incomplete feedback control of linear stochastic systems (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by Robert E. Heath and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Optimal structural design (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by Ronald A. Gellatly, Laszlo Berke, and Bell Aerospace Textron (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Optimality criteria in structural design (Wright-Patterson Air Force Base, Ohio : Air Force Systems Command, Air Force Flight Dynamics Laboratory, United States Air Force, 1971., 1971), also by William Prager, Pedro V. Marcal, and Brown University. Division of Engineering (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Optimality criterion methods in structural optimization (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by N. S. Khot and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Optimization techniques : a comparison (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States. Air Force, 1962., 1964), also by L. Schwartz and United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processes (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Optimum design of composite wing structures with twist constraint for aeroelastic tailoring (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1976., 1976), also by N. S. Khot, K. Schrader, L. Berke, V. B. Venkayya, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Panel optimization with integrated software (POIS). Volume 1, Panda -- interactive program for preliminary minimum weight design (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by D. Bushnell, Air Force Wright Aeronautical Laboratories, and Lockheed Missiles and Space Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Panel optimization with integrated software (POIS). Volume 2, User instructions -- Echo and RRSYS (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by P. Stern, P. Stehlin, Bo O. Almroth, Air Force Wright Aeronautical Laboratories, and Lockheed Missiles and Space Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Parafoil powered flight performance (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1971., 1971), also by John D. Nicolaides, Michael A. Tragarz, and University of Notre Dame. Department of Aerospace and Mechanical Engineering (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Parafoil powered flight performance (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1972., 1972), also by John D. Nicolaides and University of Notre Dame. Department of Aerospace and Mechanical Engineering (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Parafoil wind tunnel tests (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by John D. Nicolaides and University of Notre Dame. Department of Aerospace and Mechanical Engineering (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Parametric fatigue analysis of USAF aircraft (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Directorate of Laboratories, Air Force Systems Command, United States Air Force, 1967., 1967), also by George J. Roth, James C. Sliemers, John P. Ryan, and University of Dayton. Research Institute (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Post stall maneuvers and thrust vectoring performance analysis (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984., 1984), also by L. Earl Miller and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Powered parafoil systems (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), also by John D. Nicolaides and University of Notre Dame (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Prediction of creep effects in aircraft structures. Part 2 (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by C. W. Alesch, W. Robe, B. Klein, United States. Air Force. Systems Command. Aeronautical Systems Division, and General Dynamics Corporation. Convair Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Prediction of pressure fuctuations associated with maneuvering re-entry weapons. Volume 1 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by Anthony L. Laganelli, John R. Howe, United States. Air Force. Systems Command, and General Electric Company. Re-entry and Environmental Systems Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Prediction of six-degree-of-freedom store separation trajectories at speeds up to the critical speed. Volume I, Theoretical methods and comparisons with experiment (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1974, 1974), also by Frederick K. Goodwin, Jack Norman Nielsen, Marnix F. E. Dillenius, Nielsen Engineering & Research, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Prediction of six-degree-of-freedom store separation trajectories at speeds up to the critical speed. Volume II, Users manual for the computer programs (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1974., 1974), also by Frederick K. Goodwin, Marnix F. E. Dillenius, Nielsen Engineering & Research, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Prediction of the pressure oscillations in cavities exposed to aerodynamic flow (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1975., 1975), also by D. L. Smith and L. L. Shaw (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Prediction of turbulent skin friction for two-dimensional, rib-type surface roughness using a discrete element approach (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), also by Robert P. Taylor, Hugh W. Coleman, B. K. Hodge, Air Force Wright Aeronautical Laboratories, and Rockwell International (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Prediction of unsteady aerodynamic loadings on non-planar wings and wing-tail configurations in supersonic flow. Part II, Computer program description (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by Gordon D. Kramer, George E. Keylon, United States. Air Force. Systems Command, and Boeing Company. Commercial Airplane Group (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Prediction of unsteady aerodynamic loadings on non-planar wings and wing-tail configurations in supersonic flow. Part I, Theoretical development, program usage, and application (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by Jack Morito, John R. Hogley, Christopher J. Borland, United States. Air Force. Systems Command, and Boeing Company. Commercial Airplane Group (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Predictive methods for the dynamic response of a quad tilt-duct V/STOL aircraft in transition (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), also by Irving Carl Statler, A. Sowyrda, J. C. Erickson, G. Kurylowich, and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Preliminary design aerodynamic prediction methodology for missiles with nose bluntness (Wright-Patterson Air Force Base : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1978., 1978), also by Charles W. Ingram, David Shida, Carter J. Dinkeloo, Karlheinz O. W. Ball, and Systems Research Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Preliminary design and experimental investigation of the FDL-5A unmanned high L/D spacecraft. Part III, Aerodynamics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by C. F. Ehrlich, C. M. Onspaugh, R. S. Peyton, J. J. Rising, and Lockheed-California Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Preliminary design and experimental investigation of the FDL-5A unmanned high L/D spacecraft.. Part IV, Aerothermodynamics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by F. L. Guard, H. D. Schultz, and Lockheed-California Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Preliminary design of wings. Volume I, Design philosophy (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), also by Harold Switzky and Fairchild Republic Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Preliminary design of wings. Volume II, Preliminary fatigue design (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), also by Harold Switzky and Fairchild Republic Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Preliminary design of wings. Volume III, Minimum weight design of stiffened plate (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), also by Harold Switzky and Fairchild Republic Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Preliminary design of wings. Volume IV, Minimum weight design of composite structure (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), also by Harold Switzky and Fairchild Republic Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Pressure and heat transfer measurements at mach 13 and 19 for flows ahead of ramps, over expansion corners, and past fin-plate combinations : part of an investigation of hypersonic flow separation and control characteristics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by Stavros A. Hartofilis, United States. Air Force. Systems Command, and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Pressure and heat transfer measurements at Mach 5 and 8 for a fin-flat plate model : part of an investigation of hypersonic flow separation and control characteristics (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by Louis G. Kaufman, Lawrence Meckler, United States. Air Force. Systems Command. Aeronautical Systems Division, Grumman Aircraft Engineering Corporation. Research Department, and Wright-Patterson Air Force Base (Ohio) (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Pressure and heat transfer measurements for hypersonic flows over expansion corners and ahead of ramps (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1963), also by Louis G. Kaufman, United States. Air Force. Systems Command. Aeronautical Systems Division, and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Pressure and heat transfer measurements for Mach 21 flows over a blunt pyramidal configuration with aerodynamic controls : part of an investigation of hypersonic flow separation and control characteristics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by Louis G. Kaufman, United States. Air Force. Systems Command, Grumman Aircraft Engineering Corporation. Research Department, and Grumman Aircraft Engineering Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Pressure and heat transfer measurements for Mach 8 flows over a blunt pryamidal configuration with aerodynamic controls. Part I. Pressure data for delta wing surface (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by Louis G. Kaufman, United States. Air Force. Systems Command, and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Pressure and heat transfer measurements for Mach 8 flows over a blunt pyramidal configuration with aerodynamic controls (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by Louis G. Kaufman, United States. Air Force. Systems Command, and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Pressure cycling fatigue tests of F-111 crew module glass transparencies (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by George R. Holderby and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Pressure gradient effects on supersonic boundary layer turbulence : final report (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1979., 1979), also by A. J. Laderman and Ford Aerospace & Communications Corporation. Fluid Mechanics Section (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Pressure measurements at Mach 8 on an aerodynamically controllable winged re-entry configuration : part of an investigation of hypersonic flow separation and control characteristics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by Lawrence Meckler, United States. Air Force. Systems Command, and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Pressure measurements for Mach 8 flows over expansion corners and ramps on an internally cooled model. Part 2. Flows over a flat plate with and without a partial span ramp : part of an investigation of hypersonic flow separation and control characteristics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by Louis G. Kaufman, United States. Air Force. Systems Command, and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Pressure measurements for Mach 8 flows over expansion corners and ramps on an internally cooled model. Part 3 Flows over full span ramps mounted on a flat plate (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by Louis G. Kaufman, United States. Air Force. Systems Command, and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Pressure measurements for Mach 8 flows over expansion corners and ramps on an internally cooled model. Part I. Expansion corner flows part of an investigation of hypersonic flow separation and control characteristics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by Louis G. Kaufman, United States. Air Force. Systems Command, and Grumann Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Pressure measurements for Mach five flows over a blunt pyramidal configuration with aerodynamic controls : part of an investigation of hypersonic flow separation and control characteristics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by Louis G. Kaufman, United States. Air Force. Systems Command, and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Pressure measurements for mach five flows over winged re-entry configurations with aerodynamic controls. Part II. Conical cabin configuration (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by Louis G. Kaufman, United States. Air Force. Systems Command, and Grumman Aircraft Engineering Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Pressure measurements for mach five flows over winged re-entry configurations with aerodynamic controls. Part 1. Blunt cabin configuration (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by Louis G. Kaufman, Wright-Patterson Air Force Base. Flight Dynamics Laboratory. Research and Technology Division, and Grumman Aircraft Engineering Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Proceedings : ejector workshop for aerospace applications (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by R. P. Braden, H. J. P. von Ohain, K. S. Nagaraja, Air Force Wright Aeronautical Laboratories, and University of Dayton. Research Institute (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Proceedings of Damping '89 : 8-10 February 1989, West Palm Beach, Florida : final report for period Feb. 86 to Feb. 89 (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1989, 1989), also by Fla.) Damping '89 (1989 : West Palm Beach, Wright-Patterson Air Force Base (Ohio), and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Proceedings of the AFFDL/NASA/FAA wake turbulence workshop : 4-5 June 1974. (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Control Criteria Branch, Flight Control Division, Stability and Control Group, Air Force Systems Command, United States Air Force, 1975., 1974), also by F. L. Paillet (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Proceedings of the Air Force Conference on Fatigue and Fracture of Aircraft Structures and Materials : proceedings of the conference held at Miami Beach, Florida, 15-18 December 1969 (Air Force Flight Dynamics Laboratory, 1971), also by H. A. Wood, Air Force Materials Laboratory (U.S.), and Fla.) Air Force Conference on Fatigue and Fracture of Aircraft Structures and Materials (1969 : Miami Beach (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Proceedings of the Optimum System Synthesis Conference, 11-13 September 1962. (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by Ohio) Optimum System Synthesis Conference (1962 : Wright-Patterson Air Force Base and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Proceedings of the Second Conference on Matrix Methods in Structural Mechanics : proceedings of the conference held at Wright-Patterson Air Force Base, Ohio, 15-17 October 1968 (Air Force Dynamics Laboratory, Wright-Patterson Air Force Base, 1969), also by Ohio) Conference on Matrix Methods in Structural Mechanics (2nd : 1968 : Wright-Patterson Air Force Base and L. Berke (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Proceedings of the Third Conference on Matrix Methods in Structural Mechanics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973, i.e. 1974., 1973), also by Ohio) Conference on Matrix Methods in Structural Mechanics (3rd : 1971 : Wright-Patterson Air Force Base, United States. Air Force. Systems Command, and Air Force Institute of Technology (U.S.) (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Proceedings of the USAF-SwRI Aerospace Bearing Conference (Defense Documentation Center, 1964), also by Tex.) USAF-SwRI Aerospace Bearing Conference (1964 : San Antonio, Pei Moo Ku, and Southwest Research Institute (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Proceedings of the workshop on multivariable control systems (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1983., 1983), also by Michael A. Masi, Daniel E. Russ, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Proposed MIL standard and handbook : flying qualities of air vehicles (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1082., 1982), also by Roger H. Hoh, John Hodgkinson, Robert K. Heffley, Richard H. Klein, Irving L. Ashkenas, David G. Mitchell, Air Force Wright Aeronautical Laboratories, and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Quantitative feedback theory (QFT) : technique for designing multivariable control systems (Wright-Patterson AFB, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, [1987], 1987), also by Constantine H. Houpis, Isaac M. Horowitz, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Quasi-three-dimensional supersonic viscid/inviscid interactions : including separation effects : final report for period, 1 October 1972- 30 September 1975 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1975., 1975), also by Veer N. Vetsa, M. J. Werle, United States. Air Force. Systems Command, and University of Cincinnati. Aerospace Engineering Department (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Rapid evaluation of propulsion system effects. Volume III, Derivative procedure (DERIVP) users manual (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1978., 1978), also by T. E. Hickcox, W. H. Ball, R. A. Atkins, United States. Air Force. Systems Command, and Boeing Aerospace Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A rational method for predicting alighting gear dynamic loads. Volume 1, General methods (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1963., 1963), also by T. R. Ferguson, W. W. Kitts, J. Mollick, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A rational method for predicting alighting gear dynamic loads. Volume 2, Examples (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1963., 1963), also by T. R. Ferguson, W. W. Kitts, J. Mollick, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Re-entry vehicle control system design and mechanization (Wright-Patterson Air Force Base, Ohio: Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by D. K. Scharmack, M. D. Ward, and Honeywell Inc (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Real-time optimal control and differential game aircraft control algorithms for one-on-one combat (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by Gerald M. Anderson, Air Force Wright Aeronautical Laboratories, and Orincon Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Recovery system design guide (Wright-Patterson Air Force Base, Ohio : [Dept. of Defense], Dept. of the Air Force, Systems Command, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory, 1978 i.e. 1979., 1979), also by E. G. Ewing, T. W. Knacke, H. W. Bixby, and Irvin Industries Inc. California Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Recovery systems design guide (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1978., 1978), also by E. G. Ewing, T. W. Knacke, H. W. Bixby, and Irvin Industries Inc. California Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Relative transition probability and pressure broadening parameters of copper atomic lines (Air Force Flight Dynamics Laboratory, Air Force Systems Command, U. S. Air Force ;, 1978), also by Calspan Corporation and D. W. Boyer (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Research on techniques of establishing random type fatigue curves for broad band sonic loading (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by J. R. Fuller, United States. Air Force. Systems Command. Aeronautical Systems Division, and Boeing Company. Transport Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Response of aircraft encountering aircraft wake turbulence (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), also by Robert C. Nelson (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Response of nonlinear structural panels subjected to high intensity noise (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by C. Mei, Air Force Wright Aeronautical Laboratories, and University of Missouri--Rolla. Mechanical Engineering Department (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Roll handling qualities (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by I. L. Ashkenas, Wright-Patterson Air Force Base (Ohio), and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A Selective bibliography on high-angle-of-attack aerodynamics of aircraft and aircraft components at subsonic speeds (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Control Criteria Branch, Flight Control Division, Air Force Systems Command, United States Air Force, 1974., 1974), also by Henry W. Woolard (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Semielliptical cracks along holes in plates and lugs (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), also by A. F. Grandt, D. E. |q Tritsch, J. A. Harter, Air Force Wright Aeronautical Laboratories, and Purdue University. School of Aeronautics and Astronautics (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Similarity parameters and their sensitivity for transonic airframe exhaust nozzle interactions (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by Gerald Roffe, Gabriel Miller, Advanced Technology Laboratories, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Similarity studies for dissociating gases in hypersonic, low density flow (Wright Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1960., 1960), also by K. Pearce, R. J. Whalen, S. Samet, United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Six-Degree-of-Freedom flight path study generalized computer program (SDFCP) User's manual (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1975., 1975), also by Fay O. Young (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Skin friction, heat transfer, and pressure measurements on hypersonic inlet compression surfaces in the Mach number range 7.5 to 16 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1965., 1965), also by M. O. Ryder and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Skin friction measurements at a Mach number of three and momentum thickness Reynolds numbers up to a half million (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1980., 1980), also by Anthony W. Fiore (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Small disturbance transonic flows about oscillating airfoils (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), also by R. M. Traci, H. K. Cheng, J. L Farr, E. D. Albano, and inc Science Applications (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Solar thermionic electrical power system (Wright-Patterson Air Force Base, Ohio : Flight Accessories Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by D. L. Cuthbert, E. Baum, D. Jones, R. Luck, W. G. Flanigan, D. L. Kerr, J. A. Ruff, E. W. Williams, D. L. Purdy, United States. Air Force. Systems Command. Aeronautical Systems Division, and General Electric Company. Missile and Space Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Sonic fatigue design techniques for advanced composite aircraft structures : final report (Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1980), also by I. Holehouse (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Sonic fatigue design techniques for advanced composite aircraft structures : Final report (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by Ian Holehouse, Air Force Wright Aeronautical Laboratories, and Inc Rohr Industries (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A Source-Doublet approach to modeling triple ejector rack store configurations and force calculations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by Calvin L. Dyer, Charles B. Heath, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Space radiator analysis and design : Part 1 (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Donald Bawden Mackay, C. P. Bacha, United States. Air Force. Systems Command. Aeronautical Systems Division, and Inc. Space and Information Systems Division North American Aviation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Space radiator analysis and design : Part 2 (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1962), also by Donald Bawden Mackay, United States. Air Force. Systems Command. Aeronautical Systems Division, and Inc. Space and Information Systems Division North American Aviation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Stability analysis of the compressible, adiabatic similar boundary layer equations (lower branch) (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), also by G. R. Verma, Wilbur L. Hankey, S. J. Scherr, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Stability of a pair of stationary vortices in the leeward side of a cylinder in a potential flowfield (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983, 1983), also by Shiva N. Singh, Air Force Wright Aeronautical Laboratories, and University of Kentucky. Department of Mechanical Engineering (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Stability of compressible wake and jet flows (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983, 1983), also by G. R. Verma, Wilbur L. Hankey, S. J. Scherr, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Stability of filament wound cylinders under combined loading (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by A. Holston, D. A. Stang, A. Feldman, and Martin Marietta Denver Aerospace (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Stability of highly-cooled compressible laminar boundary layers (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1976., 1976), also by Louis I. Boehman, Michael G. Mariscalco, United States. Air Force. Systems Command, and University of Dayton. Research Institute (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): State of charge indicators for nickel cadmium batteries (Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963), also by M. Lurie, R. C. Shair, Harvey N. Seiger, United States. Air Force. Systems Command. Aeronautical Systems Division, and Gulton Industries (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Static aerodynamic characteristics at Mach 5 and 8 of an aerodynamically controllable winged re-entry configuration : part of an investigation of hypersonic flow separation and control characteristics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by Lawrence Meckler, United States. Air Force. Systems Command, Wright-Patterson Air Force Base. Flight Dynamics Laboratory, and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Static and rotational aerodynamic data from O° to 90° angle of attack for a series of basic and altered forebody shapes (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Research and Development Center, Air Force Systems Command, United States Air Force, 1989., 1989), also by William Bihrle, E. Dickes, B. Barnhart, Inc Bihrle Applied Research, Wright Research and Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Statics and stability of thin-walled elastic beams. Part 1, Formulation of fundamental equations (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by E. Giangreco, M. Como, M. Capurso, and Università di Napoli (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Statics and stability of thin-walled elastic beams. Part 2, Solution of equations (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by E. Giangreco, M. Como, M. Capurso, and Università di Napoli (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The statistical nature of fatigue crack propagation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1978., 1978), also by D. A. Virkler, P. K. Goel, B. M. Hillberry, United States. Air Force. Systems Command, and Purdue University. School of Mechanical Engineering (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The statistical properties of signals and measurements of simple manual control systems (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by Jerome I. Elkind, D. Lucille Darley, United States. Air Force. Systems Command. Aeronautical Systems Division, Beranek Bolt, and Wright-Patterson Air Force Base (Ohio) (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): STOL tactical aircraft investigation - externally blown flap. Volume I, Configuration definition. Supplement I, Aerodynamic trades of flap and roll control system (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by Dirk J. Renselaer, Rockwell International. Los Angeles Aircraft Division, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): STOL tactical aircraft investigation - externally blown flap. Volume III, Performance methods and takeoff and landing rules (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by Dirk J. Renselaer, Rockwell International. Los Angeles Aircraft Division, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): STOL tactical aircraft investigation - externally blown flap. Volume V, Flight control technology. Part I, Control system mechanization trade studies (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by Robert W. Phillips, Rockwell International. Los Angeles Aircraft Division, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): STORESIM : an integrated system for multi-body cfd simulations using unstructured, adaptive grids (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1996., 1996), also by M. P. Reddy and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Strain gage techniques for internal strain measurements in boron-epoxy composites (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by R. L. Egger and Boeing Aerospace Company. Research and Engineering Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Stress analysis of a fully inflated ribless guide surface parachute (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1965., 1965), also by H. G. Heinrich, Lelan R. Jamison, and University of Minnesota (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Stress analysis of a parachute during inflation and at steady state (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by H. G. Heinrich, Lelan R. Jamison, United States. Air Force. Systems Command, and University of Minnesota. Department of Aerospace Engineering and Mechanics (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Stress and strain distribution in the vicinity of interference fit fasteners (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by Merle Allen, J. A. Ellis, United States. Air Force. Systems Command, and General Dynamics Corporation. Convair Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Structural evaluation of high strain fiber and resin composite material systems (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1986., 1986), also by David L. Buchanan, Paul S. McClellan, Air Force Wright Aeronautical Laboratories, and McDonnell Aircraft Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Structural evaluation of superplastic sluminum. Part 1. Mechanical, corrosion, metallurgical data (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), also by Hadassah C. Lipsius, Alvin Shames, Julius Stock, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Structural response of a shallow spherical shell (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), also by James L. Rudd and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Structural response of Beryllium sheet produced by three fabrication methods (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by C. J. Giemza, United States. Air Force. Systems Command. Aeronautical Systems Division, and Martin Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Study and exploratory free-flight investigation of deployable aerodynamic decelerators operating at high attitudes and at high Mach numbers (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by W. E. Nickel, L. W. Sims, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Study of a liquid metal NaK-77 for application in flight control systems. Volume III, Investigation of system applications and components (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by R. C. Kumpitsch, P. J. Kroon, J. R. Granan, General Electric Company. Light Military Electronics Department, and United States. Air Force. Systems Command. Research and Technology Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Study of a response load recorder (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by P. W. Smith, Denis U. Noiseux, C. W. Dietrich, Edward A. Starr, United States. Air Force. Systems Command. Aeronautical Systems Division, and Beranek Bolt (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Study of a sonic load recorder (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by Jay H. Ball, Edward A. Starr, Denis U. Noiseux, Norman Doelling, United States. Air Force. Systems Command. Aeronautical Systems Division, and Beranek Bolt (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A study of aerodynamic control in stalled flight long laminar separation bubble analysis (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), also by Frank A. Dvorak, D. H. Choi, Air Force Wright Aeronautical Laboratories, and Inc Analytical Methods (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A study of digitally controlled flight control actuation (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), also by Howard H. Belmont, Air Force Wright Aeronautical Laboratories, and Hydraulic Research Textron (Firm) (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A study of synthesis techniques for optimal controllers (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by B. Paiewonsky, J. McIntyre, F. Terkelsen, P. Woodrow, United States. Air Force. Systems Command. Aeronautical Systems Division, Aeronautical Research Associates of Princeton, Inc General Precision, and Wright-Patterson Air Force Base (Ohio) (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Study of the effect of free-stream turbulence upon disturbances in the pre-transitional laminar boundary layer (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by James M. Kendall, Air Force Wright Aeronautical Laboratories, and Jet Propulsion Laboratory (U.S.) (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A study of the effects of parameter variation on the flying qualities of the XV-4B V/STOL aircraft (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by Arthur G. Jones and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A study of the influence of geometry on the strength of fatigue cracked panels (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by E. K. Walker and Northrop Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A study of the parameters associated with employing laser speckle correlation fringes to measure in-plane strain (Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1972), also by Frank D. Adams (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A study of the turbulent shock wave boundary layer interaction (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by Ralph Levy, Henry McDonald, Howrd J. Gibeling, Stephen J. Shamroth, United Technologies Research Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A study to correlate flight measured helicopter vibration data and pilot comments. (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1961., 1961), also by William J. Grant, Boeing Airplane Company, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Study to determine aerodynamic characteristics on hypersonic re-entry configurations. Part II--Analytical Phase, Volume 2--Design Charts (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1962., 1962), also by Frank S. Malvestuto, Vivan E. Huggins, Jules A. Larrivee, Herbert A. Mortzschky, William L. Marcy, Phillip J. Sullivan, Lockheed Aircraft Corporation, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Subsonic and transonic similarity rules for jet-flapped wings (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1976., 1976), also by Henry W. Woolard and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Subsonic characteristics of low aspect ratios. Volume I. Data analyses and design handbook (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by Eugene L. Crosthwait, Donald D. Seath, United States. Air Force. Systems Command, and General Dynamics Corporation. Fort Worth Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Subsonic characteristics of low aspect ratios. Volume II. Wind-tunnel test results (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by J. K. Beamish, Eugene L. Crosthwait, G. J. Klein, United States. Air Force. Systems Command, and General Dynamics Corporation. Fort Worth Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Subsonic diffuser designs for interceptor applications. Volume II (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by E. David Spong, R. W. Williams, J. V. Rejeske, P. M. Doane, and McDonnell Aircraft Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Subsonic flutter characteristics of a variable sweep wing and horizontal tail combination (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), also by Walter J. Mykytow, Michael H. Shirk, Lawrence J. Huttsell, and Thomas E. Noll (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Summary of landing gear initial flaws (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by W. T. Fujimoto, J. P. Gallagher, United States. Air Force. Systems Command, and McDonnell Douglas Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Supersonic inlet investigation. Volume I, Summary report (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by T. W. Tsukahira, Gordon R. Hall, M. Yaamada, W. F. Wong, United States. Air Force. Systems Command, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Supersonic inlet investigation. Volume II, Air induction sysem dynamic simulation model (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by Nasim F. Amin, Gordon R. Hall, United States. Air Force. Systems Command, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Supersonic inlet investigation. Volume III, Wind tunnel data report (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by T. W. Tsukahira, B. G. Franco, W. F. Wong, United States. Air Force. Systems Command, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Suppression of aerodynamically induced cavity pressure oscillations (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by Leonard L. Shaw (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Supression of jet noise with emphasis on the near field (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by Kenneth M. Eldred, Miltiades G. Cottis, Myron Mann, Robert W. White, United States. Air Force. Systems Command. Aeronautical Systems Division, and Western Electro-Acoustic Laboratory (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Technique development for predicting external store aerodynamic effects on aircraft performance. (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by R. Dale Gallagher, Guillermo Jimenez, United States. Air Force. Systems Command, and LTV Aerospace Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A technique for measuring in-plane displacements by holographic interferometry (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by Frank D. Adams, Richard R. Corwin, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A technique for obtaining improved real-time holographic interferometric data using pulse modulated illumination (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Structural Analysis Group, Structures Division, Air Force Systems Command, United States Air Force, 1971., 1971), also by Frank D. Adams and Gene E. Maddux (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Techniques for measuring displacement fields of deformed bodies using holographic interferometry (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Mechanics Branch, Structures Division, Air Force Systems Command, United States Air Force, 1971., 1971), also by Gene E. Maddux and R. R. Corwin (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Telemetry transducer handbook. Volume II. Catalog (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Flight Control Laboratroy, Air Research and Development Command, United States Air Force, 1961., 1961), also by Radiation Incorporated, United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Telemetry transducer handbook. Volume II. Supplement I (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Flight Control Laboratory, Air Force Systems Command, United States Air Force, 1962., 1962), also by H. F. Fisher, Radiation Incorporated, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Temperature based stress analysis of notched members : final report, September 1976 - February 1979 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1979., 1979), also by Bela Imre Sandor, E. H. Jordan, and University of Wisconsin--Madison (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Temperature responses of composite panels (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984., 1984), also by Lit S. Han, Air Force Wright Aeronautical Laboratories, and Ohio State University. Department of Mechanical Engineering (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Tentative STOL flying qualities criteria for MIL standard and handbook (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), also by Roger H. Hoh, David G. Mitchell, Air Force Wright Aeronautical Laboratories, and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Test report on measurements of the radiated noise from a Schweizer 2-32 sailplaine with and without a wing mounted multi-strut assembly (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Aero-Acoustics Branch, Vehicle Dynamics Division, Air Force Systems Command, United States Air Force, 1973., 1973), also by Davey L. Smith, Anthony R. Bayer, Richard D. Talmadge, and Rodney P. Paxon (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Tests to determine subsonic pressures, forces and moments acting on a hypersonic re-entry configurations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by K. Mantz, R. Ross, D. B. Seager, United States. Air Force. Systems Command. Aeronautical Systems Division, and Lockheed-California Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Theoretical and experimental analysis of surface cracks emanating from fastener holes (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by F. W. Smith, T. E. Kullgren, United States. Air Force. Systems Command, and Colorado State University. Department of Mechanical Engineering (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Theoretical and experimental investigation of some new longitudinal handling qualities parameters (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by Henry R. Jex, United States. Air Force. Systems Command. Aeronautical Systems Division, and Inc Systems Technology (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Theoretical and experimental studies on airloads related to hypersonic aeroelastic problems of general slender pointed configurations (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1961., 1961), also by Garabed Zartarian, Pao Tan Hsu, United States. Air Force. Systems Command. Aeronautical Systems Division, and Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A theoretical approach to analysis and design of efficient reduced control for space structures (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Research and Development Center, Air Force Systems Command, United States Air Force, 1990., 1990), also by Hayrani Oz, Ohio State University. Department of Aeronautical and Astronautical Engineering, Wright Research and Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Theoretical studies of configurations having high lift-to-drag rations in the viscous interaction regime (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by G. DaForno and Nassau County General Applied Science Laboratories (Westbury (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Thermal conductivities and diffusivities of graphite-epoxy composites (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), also by Lit S. Han, William F. Boyes, Air Force Wright Aeronautical Laboratories, and Ohio State University. Department of Mechanical Engineering (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Thermal performance of a scramjet combustor operating at Mach 5.6 flight conditions (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1997., 1997), also by Scott D. Stouffer, Deems Shelton Emmer, Richard D. Neumann, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Thrust augmentation study of high performance ejectors (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983, 1983), also by John E. Minardi, Hans von Ohain, Air Force Wright Aeronautical Laboratories, and University of Dayton. Research Institute (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Thrust augmenting ejectors (Ames Research Center, 1979), also by Workshop on Thrust Augmenting Ejectors (1978 : Ames Research Center), A. E. Lopez, Naval Air Development Center, and Ames Research Center (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Topics on flexible airplane dynamics (Wright-Patterson Air Force Base, Ohio : AF Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by Julian Wolkovitch, R.K. Siskind, H.R. Pass, B. F. Pearce, United States. Air Force. Systems Command. Aeronautical Systems Division, Inc Systems Technology, and Wright-Patterson Air Force Base (Ohio) (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Transient analysis of heat conduction through a slab by infinite series (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966), also by Thomas N. Bernstein and Robert M. Engle (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Transient heat flow across unidirectional fibers in composites (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), also by Lit S. Han, Moshen Bashizadeh-Fakhar, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Transient heat flow along uni-directional fibers in composites (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by Lit S. Han, Air Force Wright Aeronautical Laboratories, and Ohio State University. Research Foundation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Transonic kernel function method for unsteady flow calculations using a unified linear pressure panel procedure (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by D. D. Liu, M. T. Landahl, W. S. Pi, Air Force Wright Aeronautical Laboratories, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Transonic wind tunnel tests on an oscillating wing with external stores. Part II, The clean wing (Wright-Patterson Air Force Base : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1979., 1979), also by H. Tijdeman, C. M. Siebert, P. Schippers, R. Roos, R. Poestkoke, A. J. Persoon, A. N. Kraan, J. W. G. van Nunen, and Nationaal Lucht- en Ruimtevaartlaboratorium (Netherlands) (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Turbulent boundary layer measurement techniques (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1986., 1986), also by F. Kevin Owen, A. W. Fiore, Air Force Wright Aeronautical Laboratories, and Inc Complere (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Two dimensional analysis of transient heat conduction in a sector of a hollow circular cylinder (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by J. G. Torian, G. K. Bennett, and Martin Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A two-dimensional linear elastic crack tip element for Nastran (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1986., 1986), also by Peter J. Woytowitz, Richard L. Citerley, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Two-dimensional Navier-Stokes solution of the flow over a thick supercritical airfoil with strong shock-induced separation (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1988., 1988), also by Don W. Kinsey and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Two-dimensional supersonic nonadiabatic flow and axisymmetric supersonic adiabatic and nonadiabatic flows (Wright-Patterson Air Force Base, Ohio : b Air Force Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1966., 1966), also by Jack Norman Nielsen, Frederick K. Goodwin, Larry L. Lynes, Wright-Patterson Air Force Base (Ohio), and Itek Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Uniform roughness studies (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate, Wright Laboratory, Air Force Systems Command, United States Air Force, 1992., 1992), also by David E. Klett, M. Kithcart, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, North Carolina Agricultural and Technical State University, and Wright-Patterson Air Force Base (Ohio) (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Unsteady aerodynamic pressures in transonic flow (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by L. V. Andrew and North American Rockwell Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Unsteady aerodynamics for advanced configurations. Part I. Application of the subsonic kernel function to nonplanar lifting surfaces (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by H. T. Vivian, L. V. Andrew, United States. Air Force. Systems Command, and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Unsteady aerodynamics for advanced configurations. Part II A transonic box method for planar lifting surfaces (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by E. R. Rodemich, L. V. Andrew, United States. Air Force. Systems Command, and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Unsteady aerodynamics for advanced configurations. Part III. Elliptic-conical wing in linearized unsteady transonic flow (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by E. Albano, L. V. Andrew, United States. Air Force. Systems Command, Wright-Patterson Air Force Base. Flight Dynamics Laboratory, and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Unsteady aerodynamics for advanced configurations. Part IV. Application of the supersonic mach box method to intersecting planar lifting surfaces (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by M. T. Moore, L. V. Andrew, United States. Air Force. Systems Command, and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Unsteady aerodynamics for advanced configurations. Part V. Unsteady potential flow around slender bodies at angles of attack (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by T. C. Li, United States. Air Force. Systems Command, and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Unsteady Navier-Stokes solutions for a low aspect ratio delta wing (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Laboratory, Air Force Systems Command, United States Air Force, 1990., 1990), also by Raymond E. Gordnier, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Upper and lower bounds to structural deformations by dual analysis in finite elements (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by G. Sander, B. Fraeijs de Veubeke, and Université de Liège (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The USAF Stability and Control Digital Datcom. Volume I, Users manual (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by John E. Williams, Steven R. Vukelich, McDonnell Douglas Astronautics Company-St. Louis, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The USAF Stability and Control Digital Datcom. Volume I, Users manual (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1976., 1976), also by John E. Williams, Steven R. Vukelich, McDonnell Douglas Astronautics Company-St. Louis, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The USAF Stability and Control Digital Datcom. Volume II, Implementtion of Datacom methods (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1976., 1976), also by John E. Williams, Steven R. Vukelich, McDonnell Douglas Astronautics Company-St. Louis, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The USAF Stability and Control Digital Datcom. Volume III, Pilot module (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by John E. Williams, Steven R. Vukelich, McDonnell Douglas Astronautics Company-St. Louis, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): The Use of boundary-layer suction for maintaining laminar flow downstream of a reflected incidence shock wave on a flat plate at free-stream Mach numbers 2.5, 3, and 3.5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Kármán Gas Dynamics Facility, Air Research and Development Command, United States Air Force, 1965., 1965), also by S. R. Pate, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Use of optimality criteria methods for large scale systems (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, 1974., 1974), also by L. Berke and N. S. Khot (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Use of quaternions in flight mechanics (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984., 1984), also by Wilbur L. Hankey, Stephen J. Scherr, L. Earl Miller, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Use of strained coordinate perturbation method in transonic aeroelestic computations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by P. Guruswamy, Air Force Wright Aeronautical Laboratories, and Purdue University. School of Aeronautics and Astronautics (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Use of strained coordinate perturbation method in transonic aeroelestic computations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by P. Guruswamy, Air Force Wright Aeronautical Laboratories, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): V/STOL aircraft aerodynamic prediction methods investigation. Volume 1, Theoretical development of prediction methods (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by Peter T. Wooler, Henry Ziegler, Howard R. Wasson, Myles F. Schwendemann, H. C. |q Kao, Northrop Corporation. Aircraft Division, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): V/STOL aircraft aerodynamic prediction methods investigation. Volume 2, Application of prediction methods (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by Peter T. Wooler, Henry Ziegler, Howard R. Wasson, Myles F. Schwendemann, H. C. |q Kao, Northrop Corporation. Aircraft Division, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): V/STOL aircraft aerodynamic prediction methods investigation. Volume 3, Manual for computer programs (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by Peter T. Wooler, Henry Ziegler, Howard R. Wasson, Myles F. Schwendemann, H. C. |q Kao, Northrop Corporation. Aircraft Division, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): V/STOL aircraft aerodynamic prediction methods investigation. Volume 4, Literature survey (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by Peter T. Wooler, Henry Ziegler, Howard R. Wasson, Myles F. Schwendemann, H. C. |q Kao, Northrop Corporation. Aircraft Division, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Validation of United States Air Force stability and control Datcom methodologies for straight-tapered sweptforward wings (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1985., 1985), also by Daniel G. Sharpes and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Various textile parachutes and control systems to achieve steerability (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by E. M. Linhart, C. R. Graham, V. F. Riley, United States. Air Force. Systems Command, and Northrop Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Various textile parachutes and control systems to achieve steerability (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by V. F. Riley, E. M. Linhart, United States. Air Force. Systems Command, and Northrop Corporation (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): VISCID/INVISCID separated flows (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1986., 1986), also by Tuncer Cebeci, S. M. Schimke, D. P. Mack, R. W. Clark, K. C. Chang, Air Force Wright Aeronautical Laboratories, McDonnell Aircraft Company, and Douglas Aircraft Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Viscous and interacting flow field effects : proceedings of the 9th U.S. Air Force and the Federal Republic of Germany Data Exchange Agreement Meeting (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984., 1984), also by Md.) U.S. Air Force/Federal Republic of Germany Data Exchange Agreement Meeting (9th : 1984 : Silver Springs, Anthony W. Fiore, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Visualization of the flow field about parachute canopy models and approximation of canopy pressure distributions (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by Charles A. Babish, Willard C. Hunter, and United States. Air Force. Systems Command. Research and Technology Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Vortex calculations using extended potential flow theory (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, United States Air Force, 1989, 1989), also by Robert W. Guyton, Wright Research and Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Vortex interaction on a canard-wing configuration (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1986., 1986), also by Wladimiro Calarese and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Weapon bay cavity noise environments, data correlation and prediction for the B-1 aircraft (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), also by A. G. Tipton, Air Force Wright Aeronautical Laboratories, and Rockwell International (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A wind tunnel investigation of jets exhausting into a crossflow. Volume 1, Test description and data analysis (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), also by L. B. Fricke, Henry Ziegler, Peter T. Wooler, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A wind tunnel investigation of jets exhausting into a crossflow. Volume 2, Additional data for the one-jet configuration (Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970), also by L. B. Fricke, Henry Ziegler, Peter T. Wooler, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A wind tunnel investigation of jets exhausting into a crossflow. Volume 4, Additional data for three-jet configuration (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), also by L. B. Fricke, Henry Ziegler, Peter T. Wooler, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): A wind tunnel investigation of jets exhausting into a crossflow. Volume III, Additional data for two-jet configuration (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), also by L. B. Fricke, Henry Ziegler, Peter T. Wooler, and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Wind tunnel test of an AFFDL Tactical High Altitude Penetrator (THAP) air vehicle configuration (Wright-Patterson Air Force Base : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1978., 1978), also by Russel F. Osborn and Charles R. Gallaway (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Wind tunnel/flight data correlation (u). Volume I, Final report (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Flight Mechanics Division, Air Force Systems Command, United States Air Force, 1971., 1971), also by James A. Behal, Donald E. Simons, Milo H. Belgen, and North American Rockwell Corporation. Columbus Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Wind tunnel/flight data correlation (u). Volume II, Appendix I, correlation of steady state parameters at various flight conditions (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Flight Mechanics Division, Air Force Systems Command, United States Air Force, 1971., 1971), also by James A. Behal, Donald E. Simons, Milo H. Belgen, and North American Rockwell Corporation. Columbus Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Wind tunnel/flight data correlation (u). Volume III, Appendix II, the history of instantaneous total pressure compressor face contour maps (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Flight Mechanics Division, Air Force Systems Command, United States Air Force, 1971., 1971), also by James A. Behal, Donald E. Simons, Milo H. Belgen, and North American Rockwell Corporation. Columbus Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Wind tunnel/flight data correlation (u). Volume IV, Appendix II (continued), the history of instantaneous total pressure compressor face contour maps (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Flight Mechanics Division, Air Force Systems Command, United States Air Force, 1971., 1971), also by James A. Behal, Donald E. Simons, Milo H. Belgen, and North American Rockwell Corporation. Columbus Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Wind tunnell tests of ellipical missile body configurations at Mach number 0.4 to 5.0 (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1987., 1987), also by Donald E. Shereda, Valentine. III. Dahlem, Paul F. Amidon, and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Wing roll control devices for transonic high lift conditions. Part I, Fixed wing configuration (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), also by Jack D. McAllister, Perry D. Whitten, David B. Benepe, and General Dynamics Corporation. Convair Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): Wing roll control devices for transonic high lift conditions. Part II, Variable sweep configuration (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by Jack D. McAllister, Perry D. Whitten, David B. Benepe, and General Dynamics Corporation. Convair Division (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): YC-14 interior noise measurements program (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by L. M. Butzel, United States. Air Force. Systems Command, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Air Force Flight Dynamics Laboratory (U.S.): YC-15 Interior noise measurements. technical discussion (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by James L. Warnix, Donald E. Hines, United States. Air Force. Systems Command, and Douglas Aircraft Company (page images at HathiTrust)

See also what's at your library, or elsewhere.

Help with reading books -- Report a bad link -- Suggest a new listing

Home -- Search -- New Listings -- Authors -- Titles -- Subjects -- Serials

Books -- News -- Features -- Archives -- The Inside Story

Edited by John Mark Ockerbloom (onlinebooks@pobox.upenn.edu)
OBP copyrights and licenses.