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Books about United States. Air Force. Systems Command -- Books by United States. Air Force. Systems Command

Books about United States. Air Force. Systems Command:

Books by United States. Air Force. Systems Command:

Books in the extended shelves:

• United States. Air Force. Systems Command: (U) Integral rocket-ramjet component evaluation test program. Part I. Component development and initial freejet tests (Wright-Patterson Air Force Base, Ohio : Air Force Aero Propulsion Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by C. E. Franklin, John R. Smith, H. M. Brilliant, and Air Force Aero Propulsion Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: 0.2-scale B-1 external-compression inlet verification model test at transonic and supersonic Mach numbers : phase II (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1974., 1974), also by R. C. German, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Ablation and viscous effects on the force and moment characteristics of slender cone models at Mach 10 under laminar flow conditions (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by B. J. Griffith, B. M. Majors, W. T. Strike, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Active Control for the Total-In-Flight Simulator (ACTIFS) (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by E. G. Rynaski, N. Weingarten, D. Andrisanti, Calspan Corporation, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Rockwell International. Los Angeles Aircraft Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Admittance techniques in high speed flutter model testing. part 1 : Experimental results (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Gifford W. Asher, Roy K. Watanabe, United States. Air Force. Systems Command. Aeronautical Systems Division, and Boeing Airplane Company (page images at HathiTrust)
• United States. Air Force. Systems Command: AEDC high alpha aerodynamics. (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1974., 1974), also by Inc ARO and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Aerodynamic calibration and shakedwon testing of the full-scale F-15 aircraft inlet simulator (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by W. F. Kinzey, E. S. Gall, V. O Williams, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• United States. Air Force. Systems Command: Aerodynamic characteristics of 2-, 3-, and 4-, caliber tangent-ogive cylinders with nose bluffness ratios of 0.00, 0.25, 0.50, and 0.75 at Mach numbers from 0.6 to 4.0 (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Systems Analysis and Stimulation Branch, Guided Weapons Division, Air Force Systems Command, United States Air Force, 1977., 1977), also by Carroll B. Butler, Spiros Georgios Pallas, Edward S. Sears, and Air Force Armament Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Aerodynamic characteristics of a full-scale F-101 ejection seat with an anthropomorphic dummy at free-stream Mach numbers from 0.2 to 0.8 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by Lawrence L. Galigher, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Aerodynamic characteristics of an ejection seat escape system with a stabilization parachute at Mach numbers from 0.3 through 1.2 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by David E. A. Reichenau, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Aerodynamic characteristics of low aspect ratio fins at Mach numbers from 0.80 to 1.30 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), also by D.K. Smith, R. C. German, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Aerodynamic characteristics of perforated walls for transonic wind tunnels (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by J. L. Jacocks, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Aerodynamic characteristics of several low aspect ratio stabilizer fins at Mach numbers from 0.8 to 1.3 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by J. M. Whoric, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Aerodynamic characteristics of the B-1 fuselage afterbody including simulated jet exhaust effects at Mach numbers from 0.55 to 2.20 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973, 1973), also by Earl A. Price, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Aerodynamic characteristics of the HAST missile at Mach numbers 2.25, 3.0, and 4.0 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by J. H. Jones, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Aerodynamic interference effects on various weapon shapes in the flow field of a transonic wing configuration at Mach numbers from 0.5 to 1.3 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by G. R. Mattasits, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Aerodynamic interference of two axisymmetric stores at low supersonic speeds (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Armamanet Development and Test Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by John E. Burkhalter, Fred W. Martin, Air Force Armament Laboratory, and Auburn University. Department of Aerospace Engineering (page images at HathiTrust)
• United States. Air Force. Systems Command: Aerodynamic interference of wing-pylon-body combinations at low subsonic speeds (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by Kenneth Boland Walkley, Fred W. Martin, Air Force Armament Laboratory, and Auburn University. Department of Aerospace Engineering (page images at HathiTrust)
• United States. Air Force. Systems Command: Aerodynamic investigation of submunition stabiliation, retardation and dispersion concepts (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Air Force Systems Command, United States Air Force, 1974., 1974), also by James E. Brunk and Air Force Armament Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Aerodynamic loads data on the M-117 bomb in the flow field of the triple ejection rack at Mach numbers from 0.5 to 1.3 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by Willard E. Summers, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Martin Marietta Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Martin Marietta Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Aerodynamic test and analysis of a slender generic missile configuration (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Aeromechanics Division, Air Force Systems Command, United States Air Force, 1989., 1989), also by Roger S. Gates, Mark A. Fische, John R. Cipolla, G. L. Winchenback, and Air Force Armament Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Aerodynamics of missiles wih offset fin configurations (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Aeromechanics Division, Air Force Systems Command, United States Air Force, 1989., 1989), also by Gregg L. Abate and Air Force Armament Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Aerodynamics of supersonic lifting bodies (Air Force Armament Laboratory, Armamaent Division, Air Force Systems Command, United States Air Force, 1981), also by M. C. Jischke, M. L. Rasmussen, Air Force Armament Laboratory, and Mechanical University of Oklahoma. School of Aerospace (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: A.F.H.R.L. T.R. (Air Force Human Resources Laboratory, 1968), also by Air Force Human Resources Laboratory and Air Force Human Resources Laboratory. Plans and Applications Office (page images at HathiTrust)
• United States. Air Force. Systems Command: Afterbody drag investigation of a twin-nozzle fighter-type model at Mach numbers from 0.6 to 1.5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by Earl A. Price, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Air Force Academy selection variables as predictors of success in pilot training (Lackland Air Force Base, Texas : Personnel Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Lonnie D. Valentine, United States. Air Force. Systems Command. Aeronautical Systems Division, and Personnel Research Laboratory (Lackland Air Force Base (Tex.)) (page images at HathiTrust)
• United States. Air Force. Systems Command: Air Force design manual : principles and practices for design of hardened structures (Research Directorate, Air Force Special Weapons Center, Air Force Systems Command, Kirkland Air Force Base, 1962), also by N. M. Newmark, John David Haltiwanger, and Albuquerque United States. Air Force Special Weapons Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Air Force laboratory procurement management. (For sale by the Supt. of Docs., U.S. Govt. Print. Off.], 1967) (page images at HathiTrust)
• United States. Air Force. Systems Command: Air Force research and development contracting officers' handbook. (Air Force Systems Command, 1967) (page images at HathiTrust)
• United States. Air Force. Systems Command: Air Force research on job evaluation procedures (Lackland Air Force Base, Texas : Personnel Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Raymond E. Christal, Joseph M. Madden, United States. Air Force. Systems Command. Aeronautical Systems Division, and Personnel Research Laboratory (Lackland Air Force Base (Tex.)) (page images at HathiTrust)
• United States. Air Force. Systems Command: Air Force Systems Command. (The Command, 1985) (page images at HathiTrust)
• United States. Air Force. Systems Command: Air Force Systems Command. (Office of Public Affairs, Air Force Systems Command, in the 20th century) (page images at HathiTrust)
• United States. Air Force. Systems Command: Air Force Weapons Laboratory, Kirtland Air Force Base, New Mexico ([Air Force Systems Command], 1984), also by Dolores Devlin (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Douglas Aircraft Company (page images at HathiTrust)
• United States. Air Force. Systems Command: Aircraft motion sensitivity to cross and cross-coupling damping derivatives (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by R. W. Butler, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Alumina ceramics (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by Walter H. Gitzen, Air Force Materials Laboratory (U.S.), and Ohio State University. Research Foundation (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Douglas Aircraft Company (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Bell Helicopter Company (page images at HathiTrust)
• United States. Air Force. Systems Command: An analysis of initial static pressure probe measurements in a low-density hypervelocity wind tunnel (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by David E. Boylan, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Inc Anamet Laboratories (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Analysis of the three-dimensional compressible turbulent boundary layer on a sharp cone at incidence in supersonic and hypersonic flow (Arnold Air Force Base, Tennessee : Von Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by John C. Adams, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Analysis of three-dimensional inviscid supersonic flow between a body and an outer wall : with application to a jet stretcher system (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by W. C. Armstrong, R. C. Bauer, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: An analytic investigation of accuracy requirements for onboard instrumentation and film data for dynamically scaled wind tunnel drop models (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1997., 1997), also by K. S. Keen, R. L. Arterbury, C. H. Morgret, Inc Sverdrup Technology, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Analytical and experimental thermal analysis of a guided bomb (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by W. K. Crain, R. K. Matthews, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Analytical approximation of two-dimensional separated turbulent boundary-layer velocity profiles (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by T. W. Swafford, R. K. Matthews, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Analytical description of the complete two-dimensional turbulent boundary-layer velocity profile (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by David L. Whitfield, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Analytical nodel of supersonic, turbulent, near-wake flows (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by C. E. Peters, W. J. Phares, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Analytical, numerical, and experimental results on turbulent boundary layers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by David L. Whitfield, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: An analytical study of hypersonic inlets in free-molecule flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by Max Kinslow, M. R. Busby, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Analytical study of ventilated wind tunnel boundary interference on V/STOL models including wake curvature and decay effects (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1974., 1974), also by E. M. Kraft, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Analytically and experimentally determined dynamic behavior of tethered balloons (Akron, Ohio. : Goodyear Aerospace Corporation, 1973., 1973), also by Jerome J. Vorachek, George R. Doyle, Air Force Cambridge Research Laboratories (U.S.), and Goodyear Aerospace Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Annual report / United States Air Force, Air Force Systems Command (The Command, in the 20th century) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Application of splines to the numerical solution of two-point boundary-value problems (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by Donald C. Todd, John C Adams, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: An application of the Chapman-Korst theory to supersonic nozzle-afterbody flows (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by R. C. Bauer, J. H. Fox, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Application of the vortex-lattice method to represent a jet exhausting from a flat plate into a crossflowing stream (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by F. L. Heltsley, R. L. Parker, Martin Marietta Corporation, McDonnell Douglas Corporation, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Application of transilient turbulence theory to mesoscale numerical weather forecasting (Madison, Wisconsin : University of Wisconsin, CIMSS/Department of Meteorology, 1989., 1989), also by William H. Raymond, Roland B. Stull, U.S. Air Force Geophysics Laboratory, and University of Wisconsin--Madison. Department of Meteorology (page images at HathiTrust)
• United States. Air Force. Systems Command: An approximate analysis of the shock structure in underexpanded plumes (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by C. E. Peters, W. J. Phares, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Wright State University (page images at HathiTrust)
• United States. Air Force. Systems Command: Arnold Engineering Development Center high-temperature testing capabilities (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1978., 1978), also by M. H. Trimble, R. K. Matthews, R. T. Smith, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Artificially induced boundary-layer transition on blunt-slender cones using distributed roughness and spherical-type tripping devices at hypersonic speeds (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by A. H. Boudreau, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Atmospheric Chemiluminescence : COCHISE and related experiments (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1982., 1982), also by R. A. Armstrong and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Atmospheric transmittance/radiance : computer code LOWTRAN 6 (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1983., 1983), also by F. X. Kneizys, R. W. Fenn, S. A. Clough, J. E. A. Selby, L. W. Abreu, James H. Chetwynd, W. O. Gallery, Eric P. Shettle, and U.S. Air Force Geophysics Laboratory. Optical Physics Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aerospace Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aerospace Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aerospace Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Biaxial fracture strength of brittle materials (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by Henry W. Babel, Air Force Materials Laboratory (U.S.), and Douglas Aircraft Company (page images at HathiTrust)
• United States. Air Force. Systems Command: Bibliography, with abstracts, of AFCRL publications from 1 January to 31 March 1971. (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1971., 1971), also by Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Blockage study of a 1/16-scale B-1 inlet model in the 1-ft transonic and supersonic tunnels of the Propulsion Wind Tunnel Facility (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by C. F. Anderson, F. M. Jackson, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Boundary-layer characteristics at Mach numbers 2 through 5 in the test section of the 12-inch supersonic tunnel (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by D. R. Bell, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Boundary layer parameterization for a global spectral model (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1987., 1987), also by L. Mahrt, C.-T. Chu, Paul H. Ruscher, Hua-Lu Pan, U.S. Air Force Geophysics Laboratory, and Oregon State University. Department of Atmospheric Sciences (page images at HathiTrust)
• United States. Air Force. Systems Command: Boundary-layer transition correlation on a slender cone in wind tunnels and flight for indications of flow quality (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1982., 1982), also by N. Sam Dougherty, David F. Fisher, Hugh L. Dryden Flight Research Center, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Boundary-layer transition on cones near Mach one in an aeroballistic range (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by J. Leith Potter, J. R. Myers, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and University of Toronto. Institute for Aerospace Studies (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and McDonnell Aircraft Company (page images at HathiTrust)
• United States. Air Force. Systems Command: Cable and piston drag parameter investigation for hydraulic aircraft-arresting energy absorbers (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Howard L. Peterson and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• United States. Air Force. Systems Command: Calculation of interference for a porous wall wind tunnel by the method of block cyclic reduction (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by C. F. Lo, H. N. Glassman, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), Aeronautical Research Associates of Princeton, and Grumman Aircraft Engineering Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Calculation of the boundary-layer flow in the windward symmetry plane of a spherically blunted axisymmetric body at angle of attack, including streamline-swallowing effects (Arnold Air Force Base, Tennessee : Von Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by Arloe W. Mayne, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Calculation of the boundary-layer growth in a Ludwieg tube (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by James C. Sivells, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Calibration and performance of the AEDC/VKF Tunnel C, Mach Number 4, Aerothermal Wind Tunnel (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1982., 1982), also by W. T. Strike, Calspan Field Services, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Calibration of the AEDC-PWT 16-Foot transonic tunnel aerodynamic test section at various Reynolds numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1979., 1979), also by F. M. Jackson, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Calibration of the AEDC-PWT 16-ft transonic tunnel with the propulsion test section at various Reynolds numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by F. M. Jackson, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Calibration tests of a Litton conical air data probe at Mach numbers of 2 to 8 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1962., 1962), also by Scott R. Mallard, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Captive aircraft testing at high angles of attack (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by R. W. Butler, J. P. Christopher, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Cavity Aeroacoustics (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Aerodynamics Branch, Air Force Systems Command, United States Air Force, 1990., 1990), also by Richard E. Dix, Carroll Butler, Air Force Armament Laboratory. Aeromechanics Division, and Calspan Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Changes in the nature of fluctuations of temperature and liquid water content during the lifetime of a large-scale storm (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1982., 1982), also by R. M. Dyer, Ian D. Cohen, and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Characteristic boundary conditions for ARO-1 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1983., 1983), also by Karl R. Kneile, James L. Jacocks, Donald C. Todd, Calspan Field Services, Inc Sverdrup Technology, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Characteristics of axisymmetric and two-dimensional isoenergetic jet mixing zones (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by R. C. Bauer, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• United States. Air Force. Systems Command: Chemical kinetic regimes of hypersonic flight simulation (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by Donald J. Harney and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Cluster formation in free-jet expansions (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by A. B. Bailey, R. Dawbarn, M. R. Busby, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Comments on the use of measurements of the effective moment parameter (C m alpha) (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by C. J. Welsh, Calspan Field Services, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Comparison of hotshot tunnel force, pressure heat-transfer and shock shape data with shock tunnel data (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by E. E. Edenfield, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Comparison of store trajectory and aerodynamic loads, and model flow-field characteristics obtained in the AEDC PWT/4T and VFK/A wind tunnels at Mach number 1.63 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1979., 1979), also by D. W Hill, R. H. Tolbert, J. T. Best, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Comparison of the EMI long sea path transmittance measurements with LOWTRAN 5 calculations (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1980., 1980), also by William O. Gallery and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: A comparison of transition Reynolds numbers from 12-in. and 40-in. supersonic tunnels (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by C. J. Schueler, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Comparison of two methods used to measure aerodynamic loads acting on captive store models in wind tunnel tests (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by R. E. Dix, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Comparisons of free-flight and wind tunnel data on slender cones (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by B. J. Griffith, Leo G. Siler, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Boeing Company. Wichita Division (page images at HathiTrust)
• United States. Air Force. Systems Command: A compilation of static stability and fin loads data for slender body missile models with and without tail fins and wings. Volume I (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by G. R. Gomillion, Air Force Armament Laboratory (U.S.), Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), General Dynamics Corporation. Convair Division, and Ohio) Conference on Fibrous Composites in Flight Vehicle Design ([1st] : 1972 : Dayton (page images at HathiTrust)
• United States. Air Force. Systems Command: Computation of axisymmetric separated nozzle-afterbody flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by James L. Jacocks, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: A computer study of hypersonic laminar boundary-layer/shock-wave interaction using the time-dependent compressible Navier-Stokes equations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Darman Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by B. K. Hodge, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), Wright-Patterson Air Force Base. Flight Dynamics Laboratory, Aeronautical Research Associates of Princeton, and Grumman Aircraft Engineering Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Contribution of status factors to relationships between airmen's attitudes and job performance (Lackland Air Force Base, Texas : Personnel Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Francis D. Harding, Robert A. Bottenberg, United States. Air Force. Systems Command. Aeronautical Systems Division, and Personnel Research Laboratory (Lackland Air Force Base (Tex.)) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Corrections to single-shielded total temperature probes in subsonic, supersonic, and hypersonic flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by M. O. Varner, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Correlation between various physical and chemical properties of oxide surfaces and their constitution (1961), also by Thomas J. Gray, David Benson, Samuel F. Hulbert, State University of New York College of Ceramics at Alfred University, and Aeronautical Systems Center (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Correlation of experimental and theoretical steady-state spinning motion for a current fighter airplane using rotation-balance aerodynamic data (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by T. F. Langham, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Boeing Aerospace Company (page images at HathiTrust)
• United States. Air Force. Systems Command: Critical sting length as determined by the measurement of pitch-damping derivatives for laminar, transitional, and turbulent boundary layers at Mach number 3 for reduced frequencies of 0.0033 and 0.0056 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynaqmics Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by Bob L. Uselton, Fred B. Cyran, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Cross-flow corrected axisymmetric solution for multiple body interference (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by Fred W. Martin, Air Force Armament Laboratory, and Auburn University. Department of Aerospace Engineering (page images at HathiTrust)
• United States. Air Force. Systems Command: Database for internal store carriage and jettison. Volume II, Appendix A, configuration/run number index to the WICS database (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1990., 1990), also by R. E. Dix, T. W. Dobson, Calspan Corporation, Air Force Armament Laboratory (U.S.), and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Description and capabilities of the aeroballistic research facility (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Gunsm Rockets, and Explosives Division, Air Force Systems Command, United States Air Force, 1978., 1978), also by G. L. Winchenback, Judith Sullivan Kleist, D. G. Galanos, Billy Lucas, and Air Force Armament Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and University of Minnesota. Department of Aerospace Engineering and Mechanics (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Honeywell Inc. Systems and Research Division (page images at HathiTrust)
• United States. Air Force. Systems Command: Design study of solar energy measurement techniques (Wright-Patterson Air Force Base, Ohio : Flight Accessories Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by Bernd Ross, D. B. Bickler, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Development of a command control and communications system for light aircraft (Hanscom AFB, Massachusetts : Aerospace Instrumentation Division, Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1983., 1983), also by Alan R. Griffin and U.S. Air Force Geophysics Laboratory. Aerospace Instrumentation Division (page images at HathiTrust)
• United States. Air Force. Systems Command: Development of a computer program for store airloads prediction technique (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Armamanet Development and Test Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by A. R. Rudnicki, C. J. Neitzel, M. H. McCloskey, Air Force Armament Laboratory, and Vought Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Development of screening and selection tests for women (Lackland Air Force Base, Texas : Personnel Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Jane McReynolds, United States. Air Force. Systems Command. Aeronautical Systems Division, and Personnel Research Laboratory (Lackland Air Force Base (Tex.)) (page images at HathiTrust)
• United States. Air Force. Systems Command: Development of self-report tests to measure personality factors identified from peer nominations (Lackland Air Force Base, Texas : Personnel Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Warren T. Norman, United States. Air Force. Systems Command. Aeronautical Systems Division, Personnel Research Laboratory (Lackland Air Force Base (Tex.)), and University of Michigan. Department of Psychology (page images at HathiTrust)
• United States. Air Force. Systems Command: Development of the Air Force Precommission Screening Test-62 (Lackland Air Force Base, Texas : Personnel Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Lonnie D. Valentine, United States. Air Force. Systems Command. Aeronautical Systems Division, and Personnel Research Laboratory (Lackland Air Force Base (Tex.)) (page images at HathiTrust)
• United States. Air Force. Systems Command: Development of the Airman Classification Test 1961 (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division. Air Force Systems Command, United States Air Force, 1961), also by William B. Lecznar, United States. Air Force. Systems Command. Aeronautical Systems Division, and Personnel Research Laboratory (Lackland Air Force Base (Tex.)) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Dislocation mobility and pinning in hard materials through internal friction studies (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Techology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by P. D. Southgate, K.S. Mendelson, Air Force Materials Laboratory (U.S.), and IIT Research Institute (page images at HathiTrust)
• United States. Air Force. Systems Command: Documentation of a transonic wind tunnel test to investigate the separation characteriscis of the GBU-10C/B, the CBU-58, and the BL-755 stores from the F-16 aircraft (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by J. M. Wright, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Dominance of radiated aerodynamic noise on boundary-layer transition in supersonic-hypersonic wind tunnels : theory and application (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by Samuel R. Pate, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and University of Minnesota. Department of Aerospace Engineering and Mechanics (page images at HathiTrust)
• United States. Air Force. Systems Command: Dual Maxwellian space plasma modeling by the logarithmic method (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1983., 1983), also by A. L. Besse, M. F. Tautz, A. G. Rubin, and U.S. Air Force Geophysics Laboratory. Space Physics Division (page images at HathiTrust)
• United States. Air Force. Systems Command: Dynamic stability characteristics of a10-deg cone at Mach number 10 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by A. E. Hodapp, G. E. Burt, B. L. Uselton, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: The effect of plenum volume on the test section flow characteristics of a perforated wall transonic tunnel (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1970., 1970), also by C. F. Anderson, O. P. Credle, A. Anderson, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: The effect of pressure pulsations and vibrations on fully developed pipe flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by Donald O. Barnett, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and McDonnell Douglas Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Effect of shock impingement on the heat-transfer and pressure distributions on a cylindrical-leading-edge model at Mach number 19 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by L. G. Siler, H. E. Deskins, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Effect of state of stress on the failure of metals at various temperatures (Wright-Patterson Air Force Base, Ohio : Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, 1962., 1962), also by R. M. Haythornthwaite, David R. Jenkins, Aeronautical Systems Center (U.S.), and University of Michigan (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Aeronautical Research Associates of Princeton (page images at HathiTrust)
• United States. Air Force. Systems Command: Effects of acoustic and vortical disturbances on the turbulent boundary layer at free-stream Mach number 0.5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by John A. Benek, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-California Company (page images at HathiTrust)
• United States. Air Force. Systems Command: Effects of high intensity sound on circulation of the inner ear of the guinea pig (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Farrel R. Robinson, James P. Cleary, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: The Effects of the quantity and placement of copolymer units within the polymeric chain on the crystallization phenomena in polymers (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1968., 1968), also by Leo Mandelkern, Air Force Materials Laboratory (U.S.), and Florida State University (page images at HathiTrust)
• United States. Air Force. Systems Command: Effects of thermo-mechanical variables on the texture and bend ductility of high purity beryllium sheet (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by Just Dan, M. Herman, V. V. Damiano, Air Force Materials Laboratory (U.S.), and Pa.). Research Laboratories Franklin Institute (Philadelphia (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-Georgia Company (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-Georgia Company (page images at HathiTrust)
• United States. Air Force. Systems Command: Effects of wall cooling and leading-edge blunting on ramp-induced, laminar flow separations at Mach numbers from 3 through 6 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by J. Don Gray, G. L. Winchenbach, R. W. Rhudy, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: The Electronic properties information center (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by H. Thayne Johnson, Donald L. Grigsby, Air Force Materials Laboratory (U.S.), and Hughes Aircraft Company (page images at HathiTrust)
• United States. Air Force. Systems Command: Engineering model of unsteady flow in a cavity (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1991., 1991), also by R. C. Bauer, R. E. Dix, Calspan Corporation, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Engineering properties of ceramics : databook to guide materials selection for structural applications (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by J. F. Lynch, W. H. Duckworth, C. G. Ruderer, Air Force Materials Laboratory (U.S.), and Battelle Memorial Institute (page images at HathiTrust)
• United States. Air Force. Systems Command: Equations and charts for the evaluation of the hypersonic aerodynamic characteristics of lifting configurations by the Newtonian theory (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by E. L. Clark, L. L. Trimmer, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Equations for store separation motion simulations and instrumented model data reduction (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1996., 1996), also by K. S. Keen, Calspan Corporation, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Evaluation of a method for computation of separated, turbulent, compressible boundary layers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by M. C. Altstatt, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Evaluation of an internal balance-supporting bracket simulating lug suspension for captive stores in wind tunnel tests (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by R. E. Dix, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Evaluation of boattail geometry and exhaust plume temperature effects on nozzle afterbody drag at transonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by L. L. Galigher, R. C. Bauer, Steven F. Yaros, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Evaluation of critical sting length on a 7-deg cone as determined by measurements of dynamic stability derivatives and base pressure for Mach numbers 0.2 through 1.3 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by Frederick B. Cyran, Edward J. Marquart, Bob L. Uselton, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: An evaluation of jet simulation parameters for nozzle afterbody testing at transonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by William Lee Peters, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Evaluation of Reynolds number and tunnel wall porosity effects on nozzle afterbody drag at transonic mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by C. E. Robinson, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Boeing Commercial Airplane Company (page images at HathiTrust)
• United States. Air Force. Systems Command: Evaluation of the aerodynamic interference of the tunnel 4T Captive Trajectory System on the separation characteristics of the BLU-27 store (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by Wallace Luchuk, David W Hill, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Technology Incorporated (page images at HathiTrust)
• United States. Air Force. Systems Command: Evaluation of various exhaust nozzles at free-stream Mach numbers from 0.6 to. 3.0 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1970., 1970), also by Lawrence L. Galigher, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Excitation processes in ceramics and the anomalous increase in thermal conductivity at elevated temperatures (Wright-Patterson Air Force Base, Ohio : Directorate of Materials and Proceses, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by D. H. Whitmore, Ill.) Northwestern University (Evanston, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• United States. Air Force. Systems Command: Exhaust plume temperature effects on nozzle afterbody performance over the transonic Mach number range (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1974., 1974), also by C. E. Robinson, M. Dean High, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Exhaust plume thermodynamic effects on nonaxisymmetric nozzle afterbody performance in transonic flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by C. E. Robinson, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: An experimental and analytic investigation of a transonic shock-wave/boundary-layer interaction (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by M. C. Alstatatt, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-California Company (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-California Company (page images at HathiTrust)
• United States. Air Force. Systems Command: Experimental and theoretical study of cavity acoustics (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 2000., 2000), also by R. E. Dix, R. C. Bauer, Inc Sverdrup Technology, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Experimental determination of aerodynamic drag on a blunted 10-deg cone at angles of attack in hypersonic, rarefied flow (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by David E. Boylan, William H. Sims, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and University of Minnesota. Department of Aerospace Engineering and Mechanics (page images at HathiTrust)
• United States. Air Force. Systems Command: Experimental evaluation of inlet drag characteristics in the transonic mach number regime (Wright-Patterson Air Force Base, Ohio : Air Force Aero Propulsion Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by F. D. McVey, E. J. Phillips, J. V. Rejeske, McDonnell Douglas Corporation, and Air Force Aero Propulsion Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Experimental evaluation of inlet drag characteristics in the transonic mach number regime (Wright-Patterson Air Force Base, Ohio : Air Force Aero Propulsion Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by F. D. McVey, E. J. Phillips, J. V. Rejeske, McDonnell Douglas Corporation, and Air Force Aero Propulsion Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Experimental heat transfer to blunt axisymmetric bodies near the limit of continuum flow (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1962., 1962), also by J. Leith Potter, John T. Miller, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: An experimental investigation of ducted, reactive, turbulent jet mixing with recirculation. (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by D. E. Chriss, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: An experimental investigation of multiple-choice item structure (Lackland Air Force Base, Texas : Personnel Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Bart M. Vitola, George K. Cantrell, United States. Air Force. Systems Command. Aeronautical Systems Division, and Personnel Research Laboratory (Lackland Air Force Base (Tex.)) (page images at HathiTrust)
• United States. Air Force. Systems Command: Experimental investigation of the effect of various scaling laws on the quality of the free-drop store separation simulation (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by R. A. Paulk, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Experimental method for correcting nozzle afterbody drag for the effects of jet temperature (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by W. L. Peters, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Boeing Aerospace Company (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Experimental verification of the frictional pressure drop through porous media (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Robert T. Crook and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• United States. Air Force. Systems Command: Experiments to assess the influence of changes in the tunnel wall boundary layer on transonic wall crossflow characteristics (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by R. F. Starr, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Exploratory development of resonant metal radomes (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory , Air Force Systems Command, United States Air Force, 1978., 1978), also by William R. Bushelle, L. Clyde Hoots, McDonnell Douglas Astronautics Company-St. Louis, and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-Georgia Company (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-Georgia Company (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed Palo Alto Research Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: External store airloads prediction technique. Volume I. Technical summary (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Armament Configuration Division, Air Force Systems Command, United States Air Force, 1975., 1975), also by A. R. Rudnicki, R. D. Gallagher, C. T. Alexander, E. G. Waggoner, Air Force Armament Laboratory, and LTV Aerospace Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: External store airloads prediction technique. Volume II. Detailed Data. Book 1 : initial airloads prediction (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Armament Configuration Division, Air Force Systems Command, United States Air Force, 1975., 1975), also by A. R. Rudnicki, R. D. Gallagher, C. T. Alexander, E. G. Waggoner, Air Force Armament Laboratory, and LTV Aerospace Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: External store airloads prediction technique. Volume II. Detailed Data. Book 2 : single carriage airloads predictions (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Armament Configuration Division, Air Force Systems Command, United States Air Force, 1975., 1975), also by A. R. Rudnicki, R. D. Gallagher, C. T. Alexander, E. G. Waggoner, Air Force Armament Laboratory, and LTV Aerospace Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: External store airloads prediction technique. Volume II. Detailed Data. Book 4 : MER carriage normal force and pitching moment predictions (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Armament Configuration Division, Air Force Systems Command, United States Air Force, 1975., 1975), also by A. R. Rudnicki, R. D. Gallagher, C. T. Alexander, E. G. Waggoner, Air Force Armament Laboratory, and LTV Aerospace Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: External store airloads prediction technique. Volume II. Detailed Data. Book 5 : MER carriage axial force and rolling moment predictions and TER carriage predictions (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Armament Configuration Division, Air Force Systems Command, United States Air Force, 1975., 1975), also by A. R. Rudnicki, R. D. Gallagher, C. T. Alexander, E. G. Waggoner, Air Force Armament Laboratory, and LTV Aerospace Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: External store airloads prediction technique. Volume III. Detailed Data. Book 3 : MER carriage side force and yawing moment predictions (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Armament Configuration Division, Air Force Systems Command, United States Air Force, 1975., 1975), also by A. R. Rudnicki, R. D. Gallagher, C. T. Alexander, E. G. Waggoner, Air Force Armament Laboratory, and LTV Aerospace Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Factorial structure of basic training performance variables (Lackland Air Force Base, Texas : Personnel Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Fred E. Holdrege, United States. Air Force. Systems Command. Aeronautical Systems Division, and Personnel Research Laboratory (Lackland Air Force Base (Tex.)) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Boeing Aerospace Company (page images at HathiTrust)
• United States. Air Force. Systems Command: The far infrared sky survey experiment final report (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), also by Stephan D. Price, Kandiah Shivanandan, Thomas L. Murdock, and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Final report of the Joint Logistics Commanders Electronic Systems Reliability Workshop. (Department of the Army, the Navy, and the Air Force, 1975), also by Joint Logistics Commanders Electronic Systems Reliability Workshop (1975 : Airlie House), United States. Air Force. Logistics Command, United States. Naval Material Command, and United States. Army Materiel Command (page images at HathiTrust)
• United States. Air Force. Systems Command: Finite difference schemes for the solution of the nosetip shape change equations (Los Angeles, California : Space and Missile Systems Organization, Los Angeles Air Force Station, Air Force Systems Command, United States Air Force, 1975., 1975), also by P. G. Crowell, Space and Missile Systems Organization (U.S.), and Aerospace Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aerospace Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and North American Aviation (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), Del West Engineering, and Lockheed-California Company (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), Del West Engineering, and Lockheed-California Company (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), Del West Engineering, and Lockheed-California Company (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Cornell Aeronautical Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Cornell Aeronautical Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Flow characteristics of a 12-in. intermittent supersonic tunnel (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by A. Anderson, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Flow-field characteristics and aerodynamic loads on external stores near the fuselage and wing-pylon positions of a swept-wing/fuselage model at Mach numbers of 0.4 and 0.7: phase V (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1974., 1974), also by R. H. Roberts, J. R. Myers, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Flow-field study about a hemisphere-cylinder in the transonic and low supersonic Mach number range (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by T. Hsieh, B. M. Majors, W. T. Strike, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: A flow visualization investigation on selected shapes with emphasis on flow separation (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Armament Division, Air Force Systems Command, United States Air Force, 1983., 1983), also by M. H. Clarkson, Air Force Armament Laboratory, and University of Florida. Department of Engineering Sciences (page images at HathiTrust)
• United States. Air Force. Systems Command: Flow visualization photographs of a yawed tangent ogive cylinder at Mach number 2 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by J. H. Jones, J. E. O'Hare, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Flow visualization techniques for use in hypersonic wind tunnels (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by R. W. Rhudy, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Force and pressure tests of an AGARD Calibration Model B at a Mach number of 10 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by R. K. Matthews, L. L Trimmer, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Force and pressure tests on cones with simulated ablated noses at Mach numbers 8 and 16 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by J. S. Hahn, H. R. Little, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Force tests of standard hypervelocity ballistic models HB-1 and HB-2 at Mach 1.5 to 10 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by J. Don Gray, E. Earl Lindsay, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Free-flight investigation of ablation effects n the stability of conical reentry configurations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by C. J. Welsh, G. L. Winchenbach, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Free flight range test of the improved 20-millimeter target practice round (PJU-5/B) (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Guns, Rockets, and Explosives Division, Air Force Systems Command, United States Air Force, 1979., 1979), also by Kenneth K. Cobb and Air Force Armament Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Free-flight range tests of spinning tubular projectiles at Mach numbers from 2.0 to 3.2 (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Guns, Rockets, and Explosives Division, Air Force Systems Command, United States Air Force, 1979., 1979), also by G. L. Winchenback, Kenneth K. Cobb, and Air Force Armament Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Free-flight range tests of the MK76 MOD 5 Navy practice bobm at Mach numbers of 0.574 to 1.113 (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Guns, Rockets, and Explosives Division, Air Force Systems Command, United States Air Force, 1979., 1979), also by G. L. Winchenback, Peter Daniels, Kenneth O. West, and Air Force Armament Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Free turbulent mixing : a critical evaluation of theory and experiment (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), also by Philip Thomas Harsha, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Fundamental studies of subsonic and transonic flow separation. Part I. First phase summary report (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by Zhengming Wu, K. Anjaneyulu, Herbert Venghaus, L. Shen, R. Nygaard, C. H. Chen, K. C. Reddy, G. M. Elfstrom, Trevor H. Moulden, University of Tennessee (System). Space Institute, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Further experiments on impact-pressure probes in a low-density, hypervelocity flow (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1962., 1962), also by A. B. Bailey, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: A further note on the familiarity effect in job evaluation (Lackland Air Force Base, Texas : Personnel Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Joseph M. Madden, United States. Air Force. Systems Command. Aeronautical Systems Division, and Personnel Research Laboratory (Lackland Air Force Base (Tex.)) (page images at HathiTrust)
• United States. Air Force. Systems Command: Fusion welding of beryllium (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by B. M. MacPherson, Wallace W. Beaver, United States. Air Force. Air Research and Development Command, Brush Beryllium Company, and United States. Air Force. Aerospace Defense Command (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and McDonnell Aircraft Company (page images at HathiTrust)
• United States. Air Force. Systems Command: Geological investigation, HRS prototype test site investigation, Laramie Range, Wyoming (Waterways Experiment Station, 1971), also by Richard W. Hunt, Richard L. Stowe, J.L. Gatz, Joseph R. Curro, Roy E. Leach, and Waterways Experiment Station (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Geophysics and space environments (Hanscom Air Force Base, 1985), also by U.S. Air Force Geophysics Laboratory and Adolph S Jursa (page images at HathiTrust)
• United States. Air Force. Systems Command: Graphic determination of coefficients of part and multiple correlation in three-variable problems (Lackland Air Force Base, Texas : Personnel Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Fred E. Holdrege, Gerald Born, United States. Air Force. Systems Command. Aeronautical Systems Division, and Personnel Research Laboratory (Lackland Air Force Base (Tex.)) (page images at HathiTrust)
• United States. Air Force. Systems Command: Heat-transfer and flow-field tests of the McDonnell Douglas-Martin Marietta space shuttle configurations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by R. K. Matthews, R. H. Eaves, W. R. Martindale, Martin Marietta Corporation, McDonnell Douglas Corporation, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Heat-transfer and flow-field tests of the North American Rockwell/ General Dynamics Convair space shuttle configurations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by W. R. Martindale, L. L. Trimmer, R. K. Matthews, North American Rockwell Corporation, General Dynamics Corporation. Convair Division, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Heat-transfer and shadowgraph tests of several elliptical lifting bodies at Mach 10 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by M. E. Hillsamer, J. P. Rhudy, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Heat transfer correlations for blunt cones at angle of attack (Los Angeles, California : Space and Missile Systems Organization, Air Force Systems Command, United States Air Force, 1971., 1971), also by George F. Widhopf, Space and Missile Systems Organization (U.S.), and Aerospace Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• United States. Air Force. Systems Command: A hierarchical grouping procedure applied to a problem of grouping profiles (Lackland Air Force Base, Texas : Personnel Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Joe H. Ward, Marion E. Hook, United States. Air Force. Systems Command. Aeronautical Systems Division, and Personnel Research Laboratory (Lackland Air Force Base (Tex.)) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-California Company (page images at HathiTrust)
• United States. Air Force. Systems Command: High altitude supersonic target (HAST) : phase III (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Armament Development and Test Center, Air Force Systems Command, United States Air Force, 1977., 1977), also by D. E. Wells, W. M. Byrne, Air Force Armament Laboratory, and Beech Aircraft Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: High latitude electron detectors on satellite P78-1 : Preliminary data results (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1981., 1981), also by Roger P. Vancour and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: High speed flow and aerodynamic heating behavior of porous fibrous structures (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Myron J. Coplan and United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processes (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: The High temperature hypersonic gasdynamics facility (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Robert W. Milling and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• United States. Air Force. Systems Command: Holographic interferometry measurements of subsonic turbulent boundary layers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1979., 1979), also by D. W. Sinclair, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Ohio State University (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and General Electric Company (page images at HathiTrust)
• United States. Air Force. Systems Command: Hypersonic force, pressure, and heat transfer investigations of sharp and blunt slender cones (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by David B. Wilkinson, Shelby A. Harrington, Cornell Aeronautical Laboratory, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Hypersonic heat transfer measurements on re-entry vehivle surfaces at high Reynolds number (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory , Air Force Systems Command, United States Air Force, 1973., 1973), also by Bryan E. Richards, Von Karman Institute for Fluid Dynamics, and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Hypersonic lifting body windward surface flow-field analysis for high angles of incidence (Arnold Air Force Base, Tennessee : Von Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by John C. Adams, William R. Martindale, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Wright Research and Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Université de Liège. Laboratoire de Techniques Aéronautiques et Spatiales (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: The Influence of high angle of attack flow pheomena on the dynamic stability of slender missiles (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Armamaent Division, Air Force Systems Command, United States Air Force, 1983., 1983), also by James M. Jenista, Robert C. Nelson, Air Force Armament Laboratory, and University of Notre Dame. |b Department of Aerospace and Mechanical Engineering (page images at HathiTrust)
• United States. Air Force. Systems Command: The influence of slight leading-edge bluntness on boundary-layer transition at a Mach number of eight (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by Jack D. Whitfield, J. Leith Potter, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: An influence of the orifice on measured pressures in rarefied flow (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by J. Leith Potter, David E. Boylan, Max Kinslow, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Influence of wind tunnel noise on the location of boundary-layer transition on a slender cone at Mach numbers from 0.2 to 5.5. Volume I, Experimental methods and summary of results (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by N. Sam Dougherty, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Influence of wind tunnel noise on the location of boundary-layer transition on a slender cone at Mach numbers from 0.2 to 5.5. Volume II, Tabulated and plotted data (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by N. Sam Dougherty, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Influence of work hardening exponent on crack propagation in high-strength materials (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1966), also by G. L. Hanna, E. A. Steigerwald, Air Force Materials Laboratory (U.S.), and TRW Inc. |b Equipment Laboratories (page images at HathiTrust)
• United States. Air Force. Systems Command: Influences of sting support on aerodynamic loads acting on captive store models (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by R. E. Dix, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Influences of sway braces and mounting gaps on the static aerodynamic loading of external stores (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by R. E. Dix, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: An infrared survey of the diffuse emission within 5 ̊of the galactic plane (Optical Physics Division, Air Force Geophysics Laboratory, Air Force Systems Command, USAF, 1980), also by Stephen D. Price and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Injection of particles through a jet nozzle laterally into a supersonic airstream (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by E. E. Hilliard, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Inlet performance characteristics of a 1/5 scale Northrop YF-17 model at transonic and supersonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1974., 1974), also by M. E. Sanders, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Inlet performance characteristics of a generalized 1/4-scale tactical aircraft models at transonic and supersonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1971., 1971), also by R. F. Lauer, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Inlet performance characteristics of a generalized 1/5.2-scale aircraft model at transonic and supersonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by Jimmy Walker, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Inlet technology for air launched missiles (U) inlet configuration definition studies. Part II. Experimental flow field definition (Wright-Patterson Air Force Base, Ohio : Air Force Aero Propulsion Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by L. C. Dunsworth, K. E. Woodgrift, Marquardt Company, and Air Force Aero Propulsion Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Inlet technology for air-launched missiles. Volume II. Forebody flow field test results (Wright-Patterson Air Force Base, Ohio : Air Force Aero Propulsion Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by Francis R. Zumpano, United Aircraft Corporation. Research Laboratories, and Air Force Aero Propulsion Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Integral analysis of ducted two-stream mixing with recirculation (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by C. E. Peters, W. J. Phares, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: An integral equation method for boundary interference in a perforated-wall wind tunnel at transonic speeds (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by E. M. Kraft, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Integral rocket-ramjet component evaluation test program (U). Part II. Altitude freejet tests (Wright-Patterson Air Force Base, Ohio : Air Force Aero Propulsion Laboratory, Air Force Systems Command, United States Air Force, 1975., 1975), also by C. E. Franklin, John R. Smith, H. M. Brilliant, and Air Force Aero Propulsion Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Integral solution of compressible turbulent boundary layers using improved velocity profiles (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by David L. Whitfield, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Interactions produced by sonic lateral jets located on surface in a supersonic stream (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by W. T. Strike, J. S. Deitering, C. J. Schueler, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Douglas Aircraft Company (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Douglas Aircraft Company (page images at HathiTrust)
• United States. Air Force. Systems Command: Interference on a model afterbody from downstream support hardware at transonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by Earl A. Price, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: An investigaion of boattail geometry and Reynolds number effects on forebody and afterbody drag at transonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by A. V. Spratley, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: An investigation of an upper stage rocket plane with external-burning thrust augmentation (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by E. E. Callens, J. Leith Potter, J. T. Miller, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Investigation of drag reduction by boundary layer suction on a 50-deg swept tapered wing at M (free-stream) = 2.5 to 4 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by S. R. Pate, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: An investigation of ducted, two-stream, variable-density, turbulent jet mixing with recirculation (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by Roy J. Schulz, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: An investigation of F-16 nozzle-afterbody forces at transonic Mach numbers with emphasis on support system interference (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), also by Earl A. Price, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Investigation of flow separation on a two-dimensional flat plate haveing a variable-san trailing-edge flap at M [free stream] = 3 and 5 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by S. R. Pate, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Investigation of intermetallic compounds for very high temperature applications (Wright-Patterson Air Force Base, Ohio, Aeronautical Systems Division, Materials Laboratory, Air Force Systems Command, United States Air Force, 1961., 1961), also by Jonathan Booker, A. James Stonehouse, Robert M. Paine, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Inc Systems Technology (page images at HathiTrust)
• United States. Air Force. Systems Command: An investigation of separated flow about a hemisphere-cylinder at 0- to 19-deg incidence in the Mach number range from 0.6 to 1.5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by T. Hsieh, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: An investigation of separated flows on two-dimensional models at Mach numbers 5 and 8 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by A. L. Baer, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: An investigation of several slotted wind tunnel wall configurations with a high disk loading V/STOL model (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), also by Travis W. Binion, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: An investigation of sting interference effects on an oscillating cone in transonic flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by Frederick B. Cyran, J. P. Christopher, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-Georgia Company (page images at HathiTrust)
• United States. Air Force. Systems Command: Investigation of subsonic annular nozzles for engine exhaust/external flow interaction studies (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by R. J. Matz, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Investigation of the effects of nose bluntness on natural and induced boundary-layer transition on axisymmetric bodies in supersonic flow (Arnold Air Force Base, Tennessee : Von Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by Jack D. Coats, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: An investigation of the half-model reflection-plane technique for dynamic stability testing at transonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by T. O. Shadow, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Inviscid and viscous hypersonic nozzle flow with finite rate chemical reactions (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by E. S. Levinsky, Jerome James Brainerd, General Dynamics Corporation. Astronautics Division, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Inviscid blunt leading effects on planar surface pressure distributions at Mach number 10 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by W. T. Strike, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Ionospheric modeling (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), also by B. S. Dandekar and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Iterative item analysis (Lackland Air Force Base, Texas : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Fred E. Col Holdrege, Gerald A3C Born, Robert H. A1C Kagihara, Harry G. MSgt Lawrence, United States. Air Force. Systems Command. Aeronautical Systems Division, and Personnel Research Laboratory (Lackland Air Force Base (Tex.)) (page images at HathiTrust)
• United States. Air Force. Systems Command: Jet simulation techniques : simulation of temperature effects by altering gas composition (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1979., 1979), also by W. L. Peters, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and University of Toronto. Institute for Aerospace Studies (page images at HathiTrust)
• United States. Air Force. Systems Command: Laminar boundary-layer separation on flared bodies at supersonic and hypersonic speeds (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1965., 1965), also by J. Don Gray, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Laminar heat transfer on sharp and blunt ten-degree cones in conical and parallel low-density flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by David E. Boylan, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Laminar, transitional, and turbulent heat transfer measurements on a yawed blunt conical nosetip (Los Angeles, California : Space and Missile Systems Organization, Los Angeles Air Force Station, Air Force Systems Command, United States Air Force, 1972., 1972), also by George F. Widhopf, Space and Missile Systems Organization (U.S.), and Aerospace Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Laser-Raman flow-field diagnostics of two large hypersonic test facilities (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), also by W. D. Williams, L. L. Price, H. M. Powell, D. A. Wagner, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Linear operators for data processing (Wright-Patterson Air Force Base, Ohio : Navigation & Guidance Laboratory, Aeronautical Systems Division. Air Force Systems Command, United States Air Force, 1962., 1962), also by Ralph E. Lane and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• United States. Air Force. Systems Command: Linearized dynamics of rotating aerospace vehicles with internal angular momenta (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Duane T. McRuer, Julian Wolkovitch, United States. Air Force. Systems Command. Aeronautical Systems Division, and Inc Systems Technology (page images at HathiTrust)
• United States. Air Force. Systems Command: Longitudinal force charactristics of two AFFDL MDF-4 high lift-to-drag configurations at Mach number 19 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by A. R. Wallace, L. G. Siler, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Longitudinal static stability and inlet drag characteristics of the McDonnell Douglas F-15 tactical fighter aircraft at Mach numbers of 1.60 and 2.20 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1971., 1971), also by F. J. Keeney, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Low-density boundary-layer modulation by suction in a hypersonic nozzle (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by Max Kinslow, J. Leith Potter, M. R. Busby, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Low-density hypervelocity wind tunnel diffuser performance (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by M. W. Milligan, J. F. Bailey, Knoxville. Department of Mechanical and Aerospace Engineering niversity of Tennessee, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: A magnetic-guideway/guided-projectile system concept for aeroballistic ranges (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by George D Arney, Charles W Pender, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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), Air University United States. Air Force. Institute of Technology, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Measurement of the pressure fluctuations in the test section of the 1-foot transonic tunnel in the frequency range from 5 to 1250 cps (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1962., 1962), also by J. E. Robertson, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: The Mechanical properties of magnesium oxide as a function of temperature (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by R. B. Day, R. J. Stokes, Air Force Materials Laboratory (U.S.), and Honeywell Systems and Research Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Mechanics of composite materials. Part I, Introduction (Wright-Patterson Air Force Base, Ohio, Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by Stephen W. Tsai and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Mechanisms of deformation in polyscrystalline magnesium oxide (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by E. M. Passmore, T. Vasilos, R. Duff, Air Force Materials Laboratory (U.S.), and Avco Corporation. Research and Advanced Development Division (page images at HathiTrust)
• United States. Air Force. Systems Command: A mehod for the prediction of the effects of free-stream disturbances on boundary-layer transition (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by J. A. Benek, M. Dean High, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Method for calculation of the one-dimensional nonequilibrium flow of a general gas mixture through a hypersonic nozzle (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1962., 1962), also by George Emanuel, Walter G. Vincenti, Stanford University. Department of Aeronautics and Astronautics, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: A method for estimating jet entrainment effects on nozzle-afterbody drag (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by R. C. Bauer, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: A method of characteristics computer program for three-dimensional supersonic internal flows (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1979., 1979), also by W. C. Armstrong, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• United States. Air Force. Systems Command: A Method to calculate uncertainties of drag coefficient wind tunnel data (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Aircraft Compatibility Branch, Munitions Division, Air Force Systems Command, United States Air Force, 1980., 1980), also by Spence E. Peters and Air Force Armament Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Mid-infrared spectral behavior of igneous rocks (Hanscom AFB, Massachusetts : Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1974., 1974), also by Graham R. Hunt, John W. Salisbury, and Air Force Cambridge Research Laboratories (U.S.). Optical Physics Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Missile aerodynamic parameter and structure identification from flight test data (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Armament Development and Test Center,Air Force Systems Command, United States Air Force, 1977., 1977), also by James E. Kain, Jang G. Lee, Charles M. Brown, Air Force Armament Laboratory, and Analytic Sciences Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Missile motion sensitivity to dynamic stability derivatives (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by T. F. Langham, E. S. Washington, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Model study of the exhaust flow noise of the proposed AEDC high Reynolds number tunnel (Arnold Air Force Base, Tennessee : Von Karman Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), also by J. E. Robertson, Wyle Laboratories, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: The modification of an information retrieval system by improving vocabulary control, indexing consistency and search capabilities (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by Edward A. Janning, Air Force Materials Laboratory (U.S.), and University of Dayton. Research Institute (page images at HathiTrust)
• United States. Air Force. Systems Command: Modifications to MacCormack's 2-D Navier-Stokes compression ramp code for application to flows with axes of symmetry and wall mass transfer (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by Richard G. Hindman, Edward J. Marquart, Bob L. Uselton, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Mutual aerodynamic interference effects for multiple bodies by the cross-flow corrections method (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Armament Configuration Division, Air Force Systems Command, United States Air Force, 1971., 1971), also by Fred W. Martin and Air Force Armament Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Mutual aerodynamic interference effects for multiple bodies of revolution and distorted bodies of revolution (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Air Force Systems Command, United States Air Force, 1976., 1976), also by Fred W. Martin, Malcolm A. Cutchins, Grady. Jr Saunders, Air Force Armament Laboratory, and Auburn University. Department of Aerospace Engineering (page images at HathiTrust)
• United States. Air Force. Systems Command: Mutual aerodynamic interference effects for two axisymmetric bodies (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by Fred W. Martin and Air Force Armament Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Nacelle afterbody drag investigation of a B-1 0.06-scale model at Mach numbers from 0.55 to 2.2 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by M. L. Homan, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: NASA CR-329 (National Aeronautics and Space Administration ;, 1965), also by Alfred G. Koestler, Manned Spacecraft Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: NEQPAK, the AEDC thermochemical nonequilibrium package : theory and use (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1994., 1994), also by J. T. Curtis, R. W. Tramel, Calspan Corporation, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Neural network study final report (The Laboratory, 1989), also by DARPA Neural Network Study (U.S.) and Lincoln Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: New horizons. (Headquarters Air Force Systems Command, 1989) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), University of Southern California, and Douglas Aircraft Company (page images at HathiTrust)
• United States. Air Force. Systems Command: Noise generation in transonic wind tunnels (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by M. O. Varner, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), Wright-Patterson Air Force Base. Flight Dynamics Laboratory, and Bell Aircraft Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Bell Aircraft Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), Wright-Patterson Air Force Base. Flight Dynamics Laboratory, and Bell Aircraft Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Wright-Patterson Air Force Base. Flight Dynamics Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: A note on the drag coefficient evaluation for conical vehicles in the low-density transitional flow regime (Los Angeles, California : Space and Missile Systems Organization, Los Angeles Air Force Station, Air Force Systems Command, United States Air Force, 1967., 1967), also by Charles R. Ortloff, Space and Missile Systems Organization (U.S.), and Aerospace Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Numerical analysis of recirculating ducted flows (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by R. J. Schulz, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Numerical analysis of turbulent separated subsonic diffuser flows (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by J. C. Chien, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Numerical calculation of the subsonic and transonic turbulent boundary layer on an infinite yawed airfoil (Arnold Air Force Base, Tennessee : Von Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by John C. Adams, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Numerical computation of subsonic conical diffuser flows with nonuniform turbulent inlet conditions (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by J. C. Chien, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Numerical index of AFSC publications : indexes. (Dept. of the Air Force, Headquarters, Air Force Systems Command, Andrews Air Force Base, 1979) (page images at HathiTrust)
• United States. Air Force. Systems Command: Numerical stability analysis of a compressor model (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1982., 1982), also by K. C. Reddy, Yeng-Yung Tsui, University of Tennessee (System). Space Institute, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Officer selection and classification tests : their development and use (Lackland Air Force Base, Texas : Personnel Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Lonnie D. Valentine, John A. Creager, United States. Air Force. Systems Command. Aeronautical Systems Division, and Personnel Research Laboratory (Lackland Air Force Base (Tex.)) (page images at HathiTrust)
• United States. Air Force. Systems Command: On the Reliability of redundant structures (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by Masanobu Shinozuka, Hiroshi Itagaki, Air Force Materials Laboratory (U.S.), and Columbia University (page images at HathiTrust)
• United States. Air Force. Systems Command: Optical turbulence forecasting : a tutorial (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1980., 1980), also by Edmond M. Dewan and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Optimum filament wound composites (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by G. P. Peterson and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• United States. Air Force. Systems Command: PEGSUS 4.0 User's Manual (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1991., 1991), also by N. E. Suhs, R. W. Tramel, Calspan Corporation, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Perforated wall noise in the AEDC-PWT 16-ft and 4-ft transonic tunnels (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), also by O. P. Credle, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Predicting achievement of cadets in their first year at the Air Force Academy : Class of 1963 (Lackland Air Force Base, Texas : Personnel Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Robert E. Miller, United States. Air Force. Systems Command. Aeronautical Systems Division, and Personnel Research Laboratory (Lackland Air Force Base (Tex.)) (page images at HathiTrust)
• United States. Air Force. Systems Command: Prediction of forces and moments on finned missiles at high angle of attack in transonic flow (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Armament Division, Air Force Systems Command, United States Air Force, 1980., 1980), also by William L. Oberkampf and Air Force Armament Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and General Electric Company. Re-entry and Environmental Systems Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Nielsen Engineering & Research (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Nielsen Engineering & Research (page images at HathiTrust)
• United States. Air Force. Systems Command: Prediction of total electron content using the international reference ionosphere (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1983., 1983), also by L. F. McNamara and U.S. Air Force Geophysics Laboratory. Space Physics Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Boeing Company. Commercial Airplane Group (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Boeing Company. Commercial Airplane Group (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), Grumman Aircraft Engineering Corporation. Research Department, and Grumman Aircraft Engineering Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Pressure distribution and flow visualization tests of a 1.5 elliptic cone at Mach 10 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by R. L. Palko, A. D. Ray, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Grumann Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Pressure tests on the standard hypervelocity ballistic model HB-2 at Mach 1.5 to 5 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by Jerry H. Jones, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Problems and procedures in maintainability (Wright-Patterson Air Force Base, Ohio, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Lynn V. Rigby, Joel I. Cooper, United States. Air Force. Systems Command. Aeronautical Systems Division, and Northrop Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Problems of response contamination in personality assessment (Lackland Air Force Base, Texas : Personnel Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Warren T. Norman, United States. Air Force. Systems Command. Aeronautical Systems Division, Personnel Research Laboratory (Lackland Air Force Base (Tex.)), and University of Michigan. Department of Psychology (page images at HathiTrust)
• United States. Air Force. Systems Command: Problems underlying the numerical integration of the chemical and vibrational rate equations in a near-equilibrium flow (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by George Emanuel, Stanford University. Department of Aeronautics and Astronautics, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Proceedings. (U. S. Govt. Print. Off., 1969), also by Air Force Science and Engineering Symposium (1968 : Colorado Springs), United States. Air Force. Office of Aerospace Research, and United States Air Force (page images at HathiTrust)
• United States. Air Force. Systems Command: Proceedings. ([Air Force Systems Command], 1962), also by Monterey California) AFSC Management Conference (1st : 1962 : U.S. Naval Postgraduate School (page images at HathiTrust)
• United States. Air Force. Systems Command: Proceedings. (United States Air Force Systems Command, 1962), also by AFSC Management Conference (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Proceedings of the STIP Symposium on Solar Radio Astronomy, Interplanetary Scintillations and Coordination with Spacecraft (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1982., 1982), also by M. A. Shea, G. J. Nelson, D. J. McLean, D. F. Smart, U.S. Air Force Geophysics Laboratory, and CSIRO Solar Radio Observatory (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Air Force Institute of Technology (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Property determinations for CFW graphite (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by R. B. Dull, Air Force Materials Laboratory (U.S.), and Union Carbide Corporation. Carbon Products Division (page images at HathiTrust)
• United States. Air Force. Systems Command: Propulsion system integration and test program (steady state) (U) summary (U). Part I. Integration technique and test activities (Wright-Patterson Air Force Base, Ohio : Air Force Aero Propulsion Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), also by Robert H. Johnson, United Aircraft Corporation. Pratt & Whitney Aircraft Division, North American Rockwell Corporation, General Motors Corporation. Allison Division, and Air Force Aero Propulsion Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Propulsion system integration and test program (steady state) (U) summary (U). Part II. Vehicle analysis studies (U) (Wright-Patterson Air Force Base, Ohio : Air Force Aero Propulsion Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), also by Robert H. Johnson, North American Rockwell Corporation, General Motors Corporation. Allison Division, and Air Force Aero Propulsion Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Propulsion system integration and test program (steady state). Part III. Nozzle interaction drag tests (Wright-Patterson Air Force Base, Ohio : Air Force Aero Propulsion Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), also by R. C. Westphal, R. H. Johnson, North American Rockwell Corporation, and Air Force Aero Propulsion Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and University of Cincinnati. Aerospace Engineering Department (page images at HathiTrust)
• United States. Air Force. Systems Command: Radiation parameterization programs for use in general circulation models (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1984., 1984), also by Kuo-Nan Liou, George Koenig, Stefan Kinne, Szu-Cheng Ou, U.S. Air Force Geophysics Laboratory, and University of Utah (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Boeing Aerospace Company (page images at HathiTrust)
• United States. Air Force. Systems Command: A regional forecasting model (Hanscom Air Force Base, Massachusetts : Geophysics Laboratory, United States Air Force Systems Command, 1990., 1990), also by W. H. Jasperson, David E. Venne, U.S. Air Force Geophysics Laboratory, and Control Data Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: The relationship of earliest failures to fleet size and "parent" population (Wright-Patterson Air Force, Ohio : Air Force Materials Laboratory, Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by Robert A. Heller, A. S. Heller, Air Force Materials Laboratory (U.S.), and Columbia University. Department of Civil Engineering and Engineering Mechanics (page images at HathiTrust)
• United States. Air Force. Systems Command: The relationship of microstructure to strength and toughness in high-strength steel (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by J. H. Bucher, J. W. Spretnak, G. W. Powell, J. C. Jasper, J. T. Cammett, Air Force Materials Laboratory (U.S.), and Ohio State University. Research Foundation (page images at HathiTrust)
• United States. Air Force. Systems Command: Relationships between personality traits, physical proficiency, and cadet effectiveness reports of Air Force Academy cadets (Lackland Air Force Base, Texas : Personnel Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Ernest C. Tupes, Margorie N. Kaplan, United States. Air Force. Systems Command. Aeronautical Systems Division, and Personnel Research Laboratory (Lackland Air Force Base (Tex.)) (page images at HathiTrust)
• United States. Air Force. Systems Command: Report on atmospheric environment interaction with free and tethered balloons (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1977., 1977), also by Robert L. Vesprini, M. Patricia Hagan, U.S. Air Force Geophysics Laboratory, and Mass.) Emmanuel College (Boston (page images at HathiTrust)
• United States. Air Force. Systems Command: Research and development on advanced graphite materials (Wright-Patterson Air Force Base, Ohio, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Parma National Carbon Company. Research Laboratory and Union Carbide Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Research and development on advanced graphite materials : Part II (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by Parma National Carbon Company. Research Laboratory, United States. Air Force. Systems Command. Aeronautical Systems Division, and Union Carbide Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Research and engineering studies and analyses of fan engine stall dynamic interaction with other subsystems and system performance / Dr. B. H. Goethert and 5 others. (Wright-Patterson Air Force Base, Ohio : Air Force Aero Propulsion Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), also by B. H. Goethert, William T. Snyder, Gerhard W. Braun, Eugene C. Huebschmann, Franz N. Fett, William F. Kimsey, University of Tennessee (System). Space Institute, and Air Force Aero Propulsion Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Research on adaptive wall wind tunnels (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1978., 1978), also by Robert J. Vidal, J. C Erickson, Arnold Engineering Development Center, and Calspan Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Research on dispersion strengthened cobalt-base alloys (Wright-Patterson Air Force, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by A. L. Mincher, Air Force Materials Laboratory (U.S.), and Dyes and Pigments Department E.I. du Pont de Nemours & Company. Chemicals (page images at HathiTrust)
• United States. Air Force. Systems Command: Research on hydrogen overvoltage on metallic single crystal (Wright-Patterson Air Force Base, Ohio : Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by R. Piontelli, A. La Vechhia, L. Peraldo Bicelli, United States. Air Force. Systems Command. Aeronautical Systems Division, and Politecnico di Milano (page images at HathiTrust)
• United States. Air Force. Systems Command: Resistivity of dense copper vapor (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1976., 1976), also by A. G. Rubin and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Results of a 0.1-scale B-1 inlet model test at transonic and supersonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), also by F. J. Graham, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Results of a 0.2-scale B-1 inlet verification model test at transonic and supersonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by John F. Riddell, F. M. Jackson, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Results of the full-scale F-15 inlet/engine compatibility test at subsonic and supersonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by H. E. McDill, J. L. Jacocks, R. F. Lauer, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Roll-damping derivative calculations for spinning sharp and blunt cones in supersonic and hypersonic flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1979., 1979), also by Arloe W. Mayne, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Separated and nonseparated turbulent flows about axisymmetric nozzle afterbodies. Part I, Detailed surface measurements (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), also by John A. Benek, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Shock-absorbing materials : report 4 : aging of backpacking materials (Waterways Experiment Station, 1968), also by G. C. Hoff, James M. Holzer, and William F. McCleese (page images at HathiTrust)
• United States. Air Force. Systems Command: Shock-fitting for full potential equation (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1978., 1978), also by M. M. Hafez, Earll M. Murman, Arnold Engineering Development Center, and inc Flow Research (page images at HathiTrust)
• United States. Air Force. Systems Command: The shock shape and shock detachment distance for spheres and flat-faced bodies in low-density, hypervelocity, argon flow (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by A. B. Bailey, W. H. Sims, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Similarity of factors underlying peer ratings of socially acceptable, socially unacceptable, and bipolar personality traits (Lackland Air Force Base, Texas : Personnel Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Ernest C. Tupes, Margorie N. Kaplan, United States. Air Force. Systems Command. Aeronautical Systems Division, and Personnel Research Laboratory (Lackland Air Force Base (Tex.)) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Advanced Technology Laboratories (page images at HathiTrust)
• United States. Air Force. Systems Command: Simplified input for certain aerodynamic nose configurations to the Grumman QUICK-geometry system : a KWIKNOSE User's Manual (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by Frederick L. Shope, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Skin-friction measurements at subsonic and transonic Mach numbers with embedded-wire gages (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by D. W. Sinclair, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Small vehicle dynamics study II : cross hatch studies (Norton Air Force Base, California : Space and Missile Systems Organization, Air Force Systems Command, United States Air Force, 1971., 1971), also by Charles O. White, Henry L. Moody, Richard M. Grabow, Space and Missile Systems Organization (U.S.), and Philco-Ford Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Solution for the transient one-dimensional heat conduction in an infinite slab (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by John T. Miller, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Spectroscopic investigation of laser-initiated low-pressure plasmas in atmospheric gases (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1982., 1982), also by R. A. Armstrong, W. T. Rawlins, R. A. Lucht, and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and University of Dayton. Research Institute (page images at HathiTrust)
• United States. Air Force. Systems Command: Stability theory for cross hatching. Part I, Linear stability theory (Norton Air Force Base, California : Space and Missile Systems Organization, Air Force Systems Command, United States Air Force, 1972., 1972), also by Lester Lees, Denny R. S. Ko, T. Kubota, Space and Missile Systems Organization (U.S.), and California Institute of Technology (page images at HathiTrust)
• United States. Air Force. Systems Command: Stability theory for cross hatching. Part II, An experiment on turbulent boundry layer over a wavy wall (Norton Air Force Base, California : Space and Missile Systems Organization, Air Force Systems Command, United States Air Force, 1972., 1972), also by Lester Lees, Asher Sigal, T. Kubota, Space and Missile Systems Organization (U.S.), and California Institute of Technology (page images at HathiTrust)
• United States. Air Force. Systems Command: Stagnation point boundary layer with large wall-to-freestream enthalpy ratio (Los Angeles, California : Space and Missile Systems Organization, Los Angeles Air Force Station, Air Force Systems Command, United States Air Force, 1967., 1967), also by Harold Mirels, William E Welsh, Space and Missile Systems Organization (U.S.), and Aerospace Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: State-of-the-art review on ferroelectric ceramic materials (Wright-Patterson Air Force Base, Ohio : Air Force Material Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by R. M. Gruver, C. W. Dickey, W. R. Buessem, Air Force Materials Laboratory (U.S.), and Pennsylvania State College (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), Wright-Patterson Air Force Base. Flight Dynamics Laboratory, and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• United States. Air Force. Systems Command: Static aerodynamic characteristics of a series of generalized slender bodies with and without fins at Mach numbers form 0.6 to 3.0 and angles of attack from 0 to 180 deg. Volume 1 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by William B. Baker, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Static force tests at Mach 8 of sharp and blunt 20-deg half-angle cones with a blunt 70-deg swept delta wing (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1962., 1962), also by G. H. Merz, O. R. Pritts, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Static pressure on sharp and blunt cones in conical and parallel low-density flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1974., 1974), also by Max Kinslow, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Static stability and drag characteristics of a hypersonic aircraft design at Mach numbers 1.5 to 5.6 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by J. T. Jr Best, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Static stability and drag characteristics of the HAST missile at Mach numbers 2.25, 3.0, and 4.0 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1974., 1974), also by J. T. Best, R. W. Rhudy, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Purdue University. School of Mechanical Engineering (page images at HathiTrust)
• United States. Air Force. Systems Command: Sting dynamics of wind tunnel models (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by James P. Billingsley, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Sting interference effects as determined by measurements of dynamic stability derivatives, surface pressure, and base pressure for Mach numbers 2 through 8 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by Bob L. Uselton, Frederick B. Cyran, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Sting interference effects on the Modified Basic Finner Missile at Mach numbers 0.3 through 1.3 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1982., 1982), also by Edward J. Marquart, Calspan Field Services, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Rockwell International. Los Angeles Aircraft Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Rockwell International. Los Angeles Aircraft Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Rockwell International. Los Angeles Aircraft Division (page images at HathiTrust)
• United States. Air Force. Systems Command: Store separation testing techniques at the Arnold Engineering Development Center. Volume I, An overview (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by J. B. Carman, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Store separation testing techniques at the Arnold Engineering Development Center. Volume II, Description of captive trajectory store separation testing in the aerodynamic wind tunnel (4T) (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by J. B. Carman, J. P. Christopher, D. W. Hill, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Store separation testing techniques at the Arnold Engineering Development Center. Volume III, Description and validation of Captive trajectory store separation testing in the Von Karman Facility. (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), also by J. P. Billingsley, J. T. Best, R. H. Burt, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Store separation testing techniques at the Arnold Engineering Development Center. Volume IV, Description of dynamic drop store separation testing (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by E. G Allee, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and University of Minnesota. Department of Aerospace Engineering and Mechanics (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and General Dynamics Corporation. Convair Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Structure and composition measurements in equatorial ionospheric bubbles (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1980., 1980), also by R. Narcisi, P. Bench, L. Wlodyka, G. Federico, Edmund Trzcinski, and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: A study of acoustic disturbances and means of suppression in ventilated transonic wind tunnel walls (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by N. Sam Dougherty, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: A study of cumulus arameterization in a global circulation model (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1985., 1985), also by Su-Tzai Soong, University of Illinois at Urbana-Champaign. Department of Atmospheric Sciences, and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: A study of penetration of a liquid injectant into a supersonic flow (Los Angeles, California : Space and Missile Systems Organization, Los Angeles Air Force Station, Air Force Systems Command, United States Air Force, 1967., 1967), also by Kenneth P. Horn, Roy E. Reichenbach, Marc A. Kolpin, Space and Missile Systems Organization (U.S.), and Aerospace Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: A study of the factors affecting the decompoisition of the intermediate phase gamma Ti3A1 (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by P. A. Farrar, H. Margolin, Air Force Materials Laboratory (U.S.), and New York University (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and United Technologies Research Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and General Dynamics Corporation. Fort Worth Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and General Dynamics Corporation. Fort Worth Division (page images at HathiTrust)
• United States. Air Force. Systems Command: Subsonic flow of hot gas through a highly cooled constant-area channel (Los Angeles, California : Space and Missile Systems Organization, Los Angeles Air Force Station, Air Force Systems Command, United States Air Force, 1967., 1967), also by Harold Mirels, Space and Missile Systems Organization (U.S.), and Aerospace Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and McDonnell Douglas Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Summary of regression analyses in the prediction of leadership criteria : Air Force Academy classes of 1961 through 1963 (Lackland Air Force Base, Texas : Personnel Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by John A. Creager, Robert E. Miller, United States. Air Force. Systems Command. Aeronautical Systems Division, and Personnel Research Laboratory (Lackland Air Force Base (Tex.)) (page images at HathiTrust)
• United States. Air Force. Systems Command: Summary report on aerodynamic characteristics of standard models HB-1 and HB-2 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by J. Don Gray, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: A superconducting magnet dewar missile for launching in ballistic ranges (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by E. E. Erickson, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Supersonic aerodynamic characteristics of the Active Laser Seeker (ALS) configuration of a proposed maneuvering air-to-air missile design (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by D. H. Fikes, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Supersonic flow measurements in the body vortex wake of an ogive nose cylinder (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Armament Development and Test Center, Air Force Systems Command, United States Air Force, 1978., 1978), also by William L. Oberkampf, T. J. Bartel, and Air Force Armament Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• United States. Air Force. Systems Command: Support interference on an ogive-cylinder model at high angle of attack in transonic flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnet Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by M. C. Altstatt, W. E. Dietz, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Surface contour measurements of a parabolic reflector antenna by photogrammetric techniques (Columbus, Ohio, 1963), also by Dean C. Merchant, Arthur J. Brandenberger, and Ohio State University. Research Foundation (page images at HathiTrust)
• United States. Air Force. Systems Command: A Survey of checkout equipment used in Air Force weapon systems : with emphasis on the man-machine relationship (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Louis T. Pope, United States. Air Force. Systems Command. Aeronautical Systems Division, and Personnel Research Laboratory (Lackland Air Force Base (Tex.)) (page images at HathiTrust)
• United States. Air Force. Systems Command: A survey of transition research at AEDC (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1977., 1977), also by Jack D. Whitfield, N. Sam Dougherty, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: System safety (Air Force Systems Command, 1974) (page images at HathiTrust)
• United States. Air Force. Systems Command: Systems management : systems engineering management procedures. (U. S. Govt. Print. Off.], 1966) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and LTV Aerospace Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Ternary phase equilibria in transition metal-boron-carbon-silicon systems. Part I, Binary systems. Volume XIV, Constitution of the Hafnium-Vanadium and Hafnium-Chromium systems (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by E. Rudy, Air Force Materials Laboratory (U.S.), and Aerojet-General Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Ternary phase equilibria in transition metal-boron-carbon-silicon systems. Part I, Binary systems. Volume XIII, The Zirconium-Silicon and Hafnium-Silicon systems (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by C. E. Brukl, Air Force Materials Laboratory (U.S.), and Aerojet-General Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Ternary phase equilibria in transition metal-boron-carbon-silicon systems. Part I, Binary systems. Volume XII, Revision of the banadium-carbon and niobium-carbon systems (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by E. Rudy, C. E. Brukl, St Windisch, Air Force Materials Laboratory (U.S.), and Aerojet-General Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Ternary phase equilibria in transition metal-boron-carbon-silicon systems. Part I, Related binary systems. Volume VII, Ti-B system (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by E. Rudy, St Windisch, Air Force Materials Laboratory (U.S.), and Aerojet-General Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Ternary phase equilibria in transition metal-boron-carbon-silicon systems. Part I, Related binary systems. Volume VI, W-C system: supplemental information on the Mo-C system (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by E. Rudy, J. R. Hoffman, St Windisch, Air Force Materials Laboratory (U.S.), and Aerojet-General Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Ternary phase equilibria in transition metal-boron-carbon-silicon systems. Part I, Related binary systems. Volume X, Systems V-B, Nb-B, and Ta-B (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by E. Rudy, St Windisch, Air Force Materials Laboratory (U.S.), and Aerojet-General Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Ternary phase equilibria in transition metal-boron-carbon-silicon systems. Part I, Related binary systems. Volume VIII, Zr-B system (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by E. Rudy, St Windisch, Air Force Materials Laboratory (U.S.), and Aerojet-General Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Ternary phase equilibria in transition metal-boron-carbon-silicon systems. Part I, Related binary systems. Volume IX, Hf-B system (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by E. Rudy, St Windisch, Air Force Materials Laboratory (U.S.), and Aerojet-General Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Ternary phase equilibria in transition metal-boron-carbon-silicon systems. Part I, Related binary systems. Volume XI, Final report on the Mo-C system (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), also by E. Rudy, J. R. Hoffman, A. J. Stosick, St Windisch, Air Force Materials Laboratory (U.S.), and Aerojet-General Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Ternary phase equilibria in transition metal-boron-carbon-silicon systems. Part II, Ternary systems. Volume I, Ta-Hf-C System (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1968., 1965), also by E. Rudy, Air Force Materials Laboratory (U.S.), and Aerojet-General Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Tests of an arresting cable "pop-up" system (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by J. A. Zdrazil, United States. Air Force. Systems Command. Aeronautical Systems Division, and Inc Research (page images at HathiTrust)
• United States. Air Force. Systems Command: Tests of the ONERA calibration models in three transonic wind tunnels (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by Travis W. Binion, Arnold Engineering Development Center, France. Office national d'études et de recherches aérospatiales, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Colorado State University. Department of Mechanical Engineering (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Theory of space charge between parallel plane electrodes (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1982., 1982), also by Christopher Sherman and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Three-dimensional laminar boundary-layer analysis of upwash patterns and entrained vortex formation on sharp cones at angle of attack (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), also by John C. Adams, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Threshold fatigue crack growth behavior (Wright-Patterson Air Force Base, Ohio : Materials Laboratory, Wright Research Development Center, Air Force Systems Command, United States Air Force, XXXX, 1989), also by F. K. Haake, Clifford G. Annis, J. W. Fischer, Gary Charles Salivar, E. H. Hindle, Wright Research Development Center, and Pratt & Whitney Aircraft Group. Government Products Division (page images at HathiTrust)
• United States. Air Force. Systems Command: Transonic scaling effect on a quasi, two-dimensional C-141 airfoil model (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by C. F. Lo, W. E. Carleton, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Transonic wing/store flow-field measurement using a laser velocimeter (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by F. L. Heltsley, D. Brayton, F. L. Crosswy, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Two-component simultaneous LDV (Laser Doppler Velocimeter) turbulence measurements in an axisymmetric nozzle afterbody subsonic flow field with a cold, underexpanded supersonic jet (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1983., 1983), also by F. L. Heltsley, F. L. Crosswy, Calspan Field Services, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Ultrasonic methods for nondestructive measurement of residual stress (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Aeronautical Systems Division, Materials Central, U.S. Air Force, 1961., 1961), also by Fred Rollins and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• United States. Air Force. Systems Command: Ultrasonic methods for the study of stress cycling effects in metals (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Materials Central, Air Force Systems Command, United States Air Force, 1961., 1961), also by Rohn Truell, William Findley, Charles Elbaum, George Watkins Anderson, Bruce Chick, Brown University. Division of Applied Mathematics, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• United States. Air Force. Systems Command: The United States Air Force Rocket Propulsion Laboratory (U.S. Air Force, Air Force Systems Command, Air Force Rocket Propulsion Laboratory, 1986) (page images at HathiTrust)
• United States. Air Force. Systems Command: Unsolicited guide proposal. (Air Force Systems Command, 1982) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), Wright-Patterson Air Force Base. Flight Dynamics Laboratory, and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: USAF PERT. (Air Force Systems Command], 1963), also by United States Air Force (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and McDonnell Douglas Astronautics Company-St. Louis (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and McDonnell Douglas Astronautics Company-St. Louis (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and McDonnell Douglas Astronautics Company-St. Louis (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and McDonnell Douglas Astronautics Company-St. Louis (page images at HathiTrust)
• United States. Air Force. Systems Command: The use of a multi-degree-of-freedom dual balance system to measure cross and cross-coupling derivatives (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1982., 1982), also by D. R. Haberman, Calspan Field Services, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Use of the flow angularity technique for predicting store separation trajectories (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Product Assurance Division, Air Force Systems Command, United States Air Force, 1971., 1971), also by Stephen C. Korn and Air Force Armament Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: User's manual : extended capability magnus rotor and ballistic body 6-DOF trajectory program (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), also by James E. Brunk and Air Force Armament Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• United States. Air Force. Systems Command: Validation and expansion of the flow angularity technique for predicting store separation trajectories (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Aircraft Compatibility and Weapons Flight Dynamics Branch, Product Assurance Division, Air Force Systems Command, United States Air Force, 1972., 1972), also by Stephen C. Korn and Air Force Armament Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Validation of Air Force classification tests against academic grades in an aviation high school (Personnel Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961), also by Lloyd G. Humphreys, United States. Air Force. Systems Command. Aeronautical Systems Division, University of Illinois at Urbana-Champaign. Department of Psychology, and Personnel Research Laboratory (Lackland Air Force Base (Tex.)) (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command: Viscous effects on zero-lift drag of slender blunt cones (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by Jack D. Whitfield, B. J. Griffith, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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 Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• United States. Air Force. Systems Command: Wake properties behind an ejection seat escape system and aerodynamic characteristics with stabilization parachutes at Mach numbers from 0.6 to 1.5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), also by David E. A. Reichenau, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Wall temperature effects on two- and three-dimensional transonic turbulent boundary layers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by J. C Adams, Arloe W Mayne, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: A wind dependent desert aerosol model: radiative properties (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1988., 1988), also by David R. Longtin, James D. Pryce, John R. Hummel, Eric P. Shettle, and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command: Wind tunnel investigation of aerodynamic loads on weapons separated from carriage under the wing of a tactical fighter aircraft at supersonic speeds (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by J. C. Donaldson, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Wind tunnel investigation of the aerodynamic hysteresis phenomenon on the F-4 aircraft and its effects on aircraft motion (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by J. F. Herman, E. S. Washington, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Wind tunnel testing of interactions of high altitude rocket plumes with the free stream (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), also by H. K. Smithson, D. L. Whitfield, L. L. Price, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Wind tunnel tests of a 0.06-scale B-1 model at Mach numbers from 0.60 to 1.60 : phase IV (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by C. J. Spurlin, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Wind tunnel tests of a full-scale air-launched cruise missile with an installed turbofan engine (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by H. E. McDill, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Systems Command: Wind tunnel tests of supersonic two-dimensional and half-axisymmetric inlet models in a nonuniform flow field at Mach numbers from 1.5 through 2.5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), also by Frederick K. Hube, Leroy M. Jenke, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: Wind tunnel tests of two-dimensional and half-axisymmetric inlet models at Mach numbers 1.5 through 3.0 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1970., 1970), also by Frederick K. Hube, Leroy M. Jenke, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Boeing Commercial Airplane Company (page images at HathiTrust)
• United States. Air Force. Systems Command: 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, Air Force Flight Dynamics Laboratory (U.S.), and Douglas Aircraft Company (page images at HathiTrust)
• United States. Air Force. Systems Command: The Year in review (The Command, in the 20th century) (page images at HathiTrust)

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