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Unsteady flow (Aerodynamics)

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Aerodynamics, Unsteady
Flow, Transient (Aerodynamics)
Flow, Unsteady (Aerodynamics)
Transient flow (Aerodynamics)
Unsteady aerodynamics

Filed under: Unsteady flow (Aerodynamics)

Application of the pressure sensitive paint technique to steady and unsteady flow (Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames REsearch Center :, 1996), by Y. Shimbo, Brian Cantwell, R. D. Mehta, and Joint Institute for Aeronautics and Acoustics (page images at HathiTrust)
Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by James T. Howlett, Samuel R. Bland, and Langley Research Center (page images at HathiTrust)
Long time behavior of unsteady flow computations (National Aeronautics and Space Administration ;, 1992), by S. I. Hariharan and United States National Aeronautics and Space Administration (page images at HathiTrust)
Generalization of the subsonic kernel function in the s-Plane, with applications to flutter analysis (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Herbert J. Cunningham, Robert N. Desmarais, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
An analytical technique for approximating unsteady aerodynamics in the time domain / H.J. Dunn. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by H. J. Dunn, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Calculation of three-dimensional unsteady transonic flows past helicopter blades (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by J. J. Chattot, Aeromechanics Laboratory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
New technique for experimental generation of two-dimensional blade-vortex interaction at low Reynolds numbers (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Earl R. Booth, James C. Yu, and Langley Research Center (page images at HathiTrust)
Compressible, unsteady lifting-surface theory for a helicopter rotor in forward flight (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Harry L. Runyan, H. Tai, and Langley Research Center (page images at HathiTrust)
Experimental transient turbine vane temperatures in a cascade for gas stream temperature cycling between 922 and 1644 K (1200 ̊and 2500 ̊F) (National Aeronautics and Space Administration ;, 1974), by Daniel J. Gauntner, Albert Kaufman, and Lewis Research Center (page images at HathiTrust)
A Pulse-forming network for particle path visualization (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Kenneth W. McAlister, Army Research and Technology Laboratories (U.S.), United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Aeromechanics Laboratory (page images at HathiTrust)
Effect of collector configuration on test section turbulence levels in an open-jet wind tunnel (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by G. S. Manuel, P. S. Barna, John K. Molloy, and Langley Research Center (page images at HathiTrust)
Pressure and heating-rate distributions on a corrugated surface in a supersonic turbulent boundary layer (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by James Wayne Sawyer and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Effect of jet exit vanes on flow pulsations in an open-jet wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by William L. Sellers and Langley Research Center (page images at HathiTrust)
Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by John T. Batina and Langley Research Center (page images at HathiTrust)
Simulation of time-varying ascent loads on arrays of shuttle tiles in a large transonic tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Percy J. Bobbitt, Richard W. Barnwell, C. L. W. Edwards, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Evaluation of a vortex model of turbulent cavity flow (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Jay C. Hardin, P. J. W. Block, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
A model for reaction rates in turbulent reacting flows (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Wallace Chinitz, John S. Evans, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Three dimensional Euler time accurate simulations of fan rotor-stator interactions (National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ;, 1990), by A. A. Boretti and Lewis Research Center. Institute for Computational Mechanics in Propulsion (page images at HathiTrust)
Comparison of experimental and theoretical turbulance reduction characteristics for screens, honeycomb, and honeycomb-screen combinations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by James Scheiman, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Steady and nonsteady supersonic turbulent afterbody flow (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Kenneth K. Yoshikawa, Alan A. Wray, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Ames Research Center (page images at HathiTrust)
Two-dimensional Euler and Navier Stokes time accurate simulations of fan rotor flows (NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion ;, 1990), by A. A. Boretti and Lewis Research Center. Institute for Computational Mechanics in Propulsion (page images at HathiTrust)
Velocity gradient method for calculating velocities in an axisymmetric annular duct (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Theodore Katsanis and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Unsteady potential flow past a propeller blade section (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Mohammad Ali Takallu, Langley Research Center, and Lockheed Engineering & Sciences Company (page images at HathiTrust)
Development and application of a method for predicting rotor free wake positions and resulting rotor blade air loads. Volume 1, Model and results (National Aeronautics and Space Administration ;, 1971), by S. G. Sadler, Langley Research Center, and Rochester Applied Sciences Associates (page images at HathiTrust)
The effects of leading-edge serrations on reducing flow unsteadiness about airfoils : an experimental and analytical investigation (National Aeronautics and Space Administration ;, 1973), by R. G. Schwind, H. J. Allen, Ames Research Center, and Nielsen Engineering & Research (page images at HathiTrust)
Separated flow over bodies of revolution using an unsteady discrete-vorticity cross wake. Part 2, Computer program description (National Aeronautics and Space Administration ;, 1974), by F. J. Marshall, F. D. Deffenbaugh, Langley Research Center, and Purdue University. School of Aeronautics and Astronautics (page images at HathiTrust)
Fluctuating surface-pressure characteristics on slender cones in subsonic, supersonic, and hypersonic Mach-number flow (National Aeronautics and Space Administration ;, 1974), by H. Heller, Anthony R. Clemente, Langley Research Center, and Beranek Bolt (page images at HathiTrust)
Analytical and experimental study of the effects of wing-body aerodynamic interaction on space shuttle subsonic flutter (National Aeronautics and Space Administration ;, 1975), by Richard R. Chipman, Frank J. Rauch, Langley Research Center, and Grumman Aerospace Corporation (page images at HathiTrust)
A general theory of unsteady compressible potential aerodynamics (National Aeronautics and Space Administration ;, 1974), by L. Morino, Langley Research Center, and Boston University. College of Engineering (page images at HathiTrust)
Acoustic radiation and surface pressure characteristics of an airfoil due to incident turbulence (National Aeronautics and Space Administration ;, 1976), by Robert W. Paterson, Roy K. Amiet, United Technologies Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Analysis of oscillatory pressure data including dynamic stall effects (National Aeronautics and Space Administration ;, 1974), by F. O. Carta, Langley Research Center, and United Aircraft Corporation. Research Laboratories (page images at HathiTrust)
The inviscid pressure field on the tip of a semi-infinite wing and its application to the formation of a tip vortex (National Aeronautics and Space Administration ;, 1976), by G. F. Hall and United States National Aeronautics and Space Administration (page images at HathiTrust)
Some remarks on the design of transonic tunnels with low levels of flow unsteadiness (National Aeronautics and Space Administration ;, 1976), by Dennis G. Mabey, Langley Research Center, and Royal Aircraft Establishment (Great Britain). Structures Dept (page images at HathiTrust)
Two dimensional aerodynamic interference effects on oscillating airfoils with flaps in ventilated subsonic wind tunnels (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Joseph Fromme, John Werth, Michael A. Golberg, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Multiple-scale turbulence modeling of boundary layer flows for scramjet applications (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 1981), by G. Fabris, R. B. Edelman, P. T. Harsha, inc. Combustion Science and Advanced Technology Dept Science Applications, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
Modification in drag of turbulent boundary layers resulting from manipulation of large-scale structures (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by T. C. Corke, Hassan M. Nagib, Y. Guezennec, Illinois Institute of Technology, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
Turbulent flow in a square-to-round transition (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by A. M. K. P. Taylor, M. Yianneskis, James H. Whitelaw, Imperial College of Science and Technology. Mechanical Engineering Dept, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
Computational flow development for unsteady viscous flows : foundation of the numerical method (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Theodore Bratanow, Thomas Spehert, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Modification of the Douglas Neumann program to improve the efficiency of predicting component interference and high lift characteristics (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by D. R. Bristow, Gordon G. Grose, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Analysis of the scramjet inlet flow field using two-dimensional Navier-Stokes equations (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1982), by Ajay Kumar, S. N. Tiwari, Old Dominion University. Research Foundation, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
A harmonic analysis method for unsteady transonic flow and its application to the flutter of airfoils (National Aeronautical and Space Administration, Scientific and Technical Information Branch ;, 1982), by F. Edward Ehlers, W. H. Weatherill, Boeing Commercial Airplane Company, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
Unsteady two dimensional airloads acting on oscillating thin airfoils in subsonic ventilated wind tunnels (National Aeronautics and Space Adiministration, Scientific and Technical Information Office ;, 1978), by Joseph Fromme, Michael Golberg, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Assessment of turbulence models for scramjet flowfields (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by M. M. Sindir, P. T. Harsha, inc. Combustion Science and Advanced Technology Dept Science Applications, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Mean velocities and Reynolds stresses in a juncture flow (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by H. McMahon, J. Hubbartt, L. Kubendran, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Georgia Institute of Technology, and Langley Research Center (page images at HathiTrust)
A linear aerodynamic analysis for unsteady transonic cascades (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Joseph M. Verdon, Joseph R. Caspar, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
Calculation of unsteady transonic aerodynamics for oscillating wings with thickness (National Aeronautics and Space Administration ;, 1975), by S. Y. Ruo, J. G. Theisen, Langley Research Center, and Lockheed-Georgia Company (page images at HathiTrust)
On the formulation of the aerodynamic characteristics in aircraft dynamics (National Aeronautics and Space Administration ;, 1976), by Murray Tobak, Lewis B. Schiff, and Ames Research Center (page images at HathiTrust)
A finite-difference analysis of the nozzle starting process in an expansion tunnel (National Aeronautics and Space Administration ;, 1975), by K. James Weilmuenster and Langley Research Center (page images at HathiTrust)
NASA TN D-6031 (National Aeronautics and Space Administration :, 1970), by Richard W. Barnwell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Laser velocimeter systems analysis applied to a flow survey above a stalled wing (National Aeronautics and Space Administration ;, 1977), by Warren H. Young, Timothy E. Hepner, James F. Meyers, Langley Directorate, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Program and charts for determining shock tube, expansion tube, and expansion tunnel flow quantities for real air (National Aeronautics and Space Administration ;, 1975), by Charles G. Miller, Sue E. Wilder, and Langley Research Center (page images at HathiTrust)
Application of a 1-strip integral method to the unsteady supersonic aerodynamics of an inclined flat surface (National Aeronautics and Space Administration :, 1972), by Robert M. Bennett, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Hypersonic and transonic buzz measurements on the lower pitch flap of M2-F2 lifting entry configuration (National Aeronautics and Space Administration ;, 1972), by Robert W. Warner, Phillip R. Wilcox, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
Experimental investigation at a Mach number of 3.11 of the lift, drag, and pitching-moment characteristics of five blunt lifting bodies (National Aeronautics and Space Administration, 1960), by William Letko and Langley Research Center (page images at HathiTrust)
An analysis of the relaxation of laminar boundary layer on a flat plate after passage of an interface with application to expansion-tube flows (National Aeronautics and Space Administration ;, 1972), by Roop N. Gupta and Langley Research Center (page images at HathiTrust)
NASA TN D-5469 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by John D. Warmbrod, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TN D-6263 (National Aeronautics and Space Administration ;, 1971), by Jon S. Pyle, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Centered 1-D unsteady expansion of a vibrationally relaxing nitrogen-oxygen mixture (National Aeronautics and Space Administration :, 1967), by Laurence N. Connor, Frances W. Taylor, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Analysis of the dynamic lateral stability of a delta-wing airplane with frequency-dependent stability derivatives (National Aeronautics and Space Administration, 1959), by Albert E. Brown, Albert A. Schy, and Langley Research Center (page images at HathiTrust)
An initial experimental study of the effect of variations in frequency and impulse on the reduction in temperature recovery factor afforded by large-scale unsteady flow (National Advisory Committee for Aeronautics, 1958), by Robert R. Howell, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
Study of unsteady flow disturbances of large and small amplitudes moving through supersonic or subsonic steady flows (National Advisory Committee for Aeronautics, 1949), by Robert V. Hess, T. Himka, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Three-dimensional, unsteady-lift problems in high-speed flight : basic concepts (National Advisory Committee for Aeronautics, 1950), by Harvard Lomax, Franklyn B. Fuller, Max A. Heaslet, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Three-dimensional unsteady lift problems in high-speed flight : the triangular wing (National Advisory Committee for Aeronautics, 1951), by Harvard Lomax, Franklyn B. Fuller, Max A. Heaslet, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Development of a numerical modeling capability for the computation of unsteady flow on the Ohio River and its major tributaries (Waterways Experiment Station ;, 1982), by Billy H. Johnson, U.S. Army Engineer Waterways Experiment Station, and United States. Army. Corps of Engineers. Ohio River Division (page images at HathiTrust)
A transient experiment using a multiple-pulse laser light source (Aberdeen, Maryland : Aberdeen Proving Ground, 1976., 1976), by Fritz H. Oertel, U.S. Army Ballistic Research Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
Unsteady supersonic flow (Headquarters, Air Research and Development Command, 1955), by John W. Miles and United States. Air Force. Air Research and Development Command (page images at HathiTrust; US access only)
Unsteady airloads on pointed airfoils and slender bodies at high mach numbers (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), by Garabed Zartarian, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Massachusetts Institute of Technology (page images at HathiTrust)
Solution of the potential equation for the unsteady flow about a triangular wing with subsonic leading edges in a supersonic main stream (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1957., 1957), by Yudell L. Luke, Frank Wagner, Geraldine V. Coombs, United States. Air Force. Air Research and Development Command, Midwest Research Institute, and Wright Air Development Center (page images at HathiTrust)
Use of strained coordinate perturbation method in transonic aeroelestic computations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), by P. Guruswamy, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Purdue University. School of Aeronautics and Astronautics (page images at HathiTrust)
Demonstration of a transonic box method for unsteady aerodynamics of planar wings (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1966., 1966), by J. J. Olsen and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
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), by William R. Wells, Air Force Flight Dynamics Laboratory (U.S.), Wright State University, and United States. Air Force. Systems Command (page images at HathiTrust)
Further studies on high-speed unsteady flow (Wright-Patterson Air Force Systems Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by Garabed Zartarian, Harry Sauerwein, United States. Air Force. Systems Command. Aeronautical Systems Division, and Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory (page images at HathiTrust)
Research on turbine rotor-stator aerodynamic interaction and rotor negative incidence stall (Wright-Patterson Air Force Base, Ohio : Aero Propulsion Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), by Robert P. Dring, J. H. Wanger, H. David Joslyn, L. W. Hardin, Air Force Wright Aeronautical Laboratories, Air Force Aero Propulsion Laboratory (U.S.), and United Technologies Research Center (page images at HathiTrust)
Small disturbance transonic flows about oscillating airfoils (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), by R. M. Traci, H. K. Cheng, J. L Farr, E. D. Albano, Air Force Flight Dynamics Laboratory (U.S.), and inc Science Applications (page images at HathiTrust)
Manipulation of airfoil response in an unsteady stream (Los Angeles, California : University of California, Los Angeles, Mechanical, Aerospace & Nuclear Engineering Department, 1996., 1996), by Chih-Ming Ho, Los Angeles. Mechanical University of California, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
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), by M. T. Moore, L. V. Andrew, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
Application of a three-dimensional steady and unsteady full potential method for transonic flow computations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984, 1984), by J. B. Malone, N. L. Sankar, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-Georgia Company (page images at HathiTrust)
Unsteady three-dimensional aerodynamic flow (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, United States Air Force, 1997., 1997), by Donald Rockwell, United States. Air Force. Office of Scientific Research, and Lehigh University. Department of Mechanical Engineering and Mechanics (page images at HathiTrust)
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), by H. T. Vivian, L. V. Andrew, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
A flexible hypersonic vehicle model developed with piston theory : preprint (Wright Patterson Air Force Base, Ohio : Air Vehicles Directorte, Air Force Research Laboratory, Air Force Materiel Command, 2006., 2006), by Michael W. Oppenheimer, David B. Doman, and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
An Analysis of wake-stator interaction in airfoil cascades (Bolling Air Force Base, D. C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1995., 1995), by M. Barnett, D. L. Sondak, United Technologies Research Center, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
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), by R. B. Hobbs, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and General Electric Company (page images at HathiTrust)
Measurement of the pressure flucuations in the test section of the 16-foot transonic circuit in the frequency range from 5 to 1000 CPS (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Research and Development Command, United States Air Force, 1961., 1961), by H. L. Chevalier, H. E. Todd, Inc ARO, United States. Air Force. Air Research and Development Command, and Arnold Engineering Development Center (page images at HathiTrust)
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), by T. C. Li, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
The AEDC three-dimensional, potential flow computer program. Volume I. Method and computer program (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), by Donald C. Todd, Inc ARO, United States. Air Force. Arnold Air Force Base, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
Unsteady stall penetration experiments at high Reynolds number (Bolling Air Force Base, D. C. : Air Force Office of Scientific Research, United States Air Force, 1987., 1987), by Peter F. Lorber, F. O. Carta, United Technologies Research Center, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
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), by Raymond E. Gordnier, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
Second moment closure modeling of complex turbulent flows (Arlington, Virginia. : Air Force Office of Scientific Research, 2007., 2007), by Sharath Girimaji, Lawrence Ukeiley, Mark N. Glauser, Jeremy T. Pinier, Texas A & M University. Aerospace Engineering Department, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Coupling linearized far-field boundary conditions with nonlinear near-field solutions in transonic flow (Bolling Air Force Base, D. C. : Air Force Office of Scientific Research, United States Air Force, 1988., 1988), by William S. Rowe, F. Edward Ehlers, Boeing Commercial Airplane Company, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Solution-adaptive calculation of unsteady blade row interactions in transonic turbomachinery (Wright-Patterson Air Force Base, Ohio : Aero Propulsion and Power Directorate, Wright Laboratory, Air Force Materiel Command, United States Air Force, 1996., 1996), by Scott M. Richardson and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
Asymptotic far field conditions for unsteady subsonic and transonic flows (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1983., 1983), by Karl Gottfried Guderley, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and University of Dayton. Research Institute (page images at HathiTrust)
The AEDC three-dimensional, potential flow computer program. Volume II. Mathematical modeling, application, and verification (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), by Richard L. Palko, Inc ARO, United States. Air Force. Arnold Air Force Base, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
Active feedback interaction with a shear layer (Bolling Air Force Base, D. C. : Air Force Office of Scientific Research, United States Air Force, 1986., 1986), by Paul E. Dimotakis, M. M. Koochesfahani, Daniel Guggenheim Aeronautical Laboratory, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Limit cycle oscillations and nonlinear aeroelastic wing response : reduced order aerodynamic models (Arlington, Virginia : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 2004., 2004), by Earl H. Dowell, Kenneth C. Hall, Pratt School of Engineering (Duke University), and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Development of LES methodology for the analysis of high-Reynolds number 2-D and 3-D dynamic stall phenomenon (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, Aerospace Sciences, 1997., 1997), by K. N. Ghia, Urmila Ghia, University of Cincinnati. Department of Aerospace Engineering and Engineering Mechanics, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
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), by E. R. Rodemich, L. V. Andrew, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
Numerical investigation of surface curvature effects in compressible turbulent flows (Bolling Air Force Base, D. C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1994., 1994), by Linda D. Kral, John F. Donovan, McDonnell Douglas Aerospace (Firm), and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
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), 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, United States. Air Force. Systems Command, and Air Force Aero Propulsion Laboratory (U.S.) (page images at HathiTrust)
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), by R. C. Bauer, R. E. Dix, Calspan Corporation, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
Calculated aerodynamics of wings in severe maneuver (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1991., 1991), by J. E. McCune, Massachusetts Institute of Technology. Department of Aeronautics and Astronautics, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Research on post-stall aerodynamics (Bolling Air Force Base, D. C. : Air Force Office of Scientific Research, United States Air Force, 1986., 1986), by R. B. Myers, S. C. Crow, Q. T. Nguyen, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Nonlinear stability of unsteady viscous flow (Ames, Iowa : Iowa State University, Contracts and Grants Office, 1995., 1995), by Alric P. Rothmayer, Iowa State University, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Experimental studies on the interaction of strong sound fields with free convection boundary layers (Wright-Patterson Air Force Base, Ohio : Aeronautical Research Laboratory, Air Force Research Division, Air Research and Development Command, United States Air Force, 1960., 1960), by E. E. Soehngen, J. P. Holman, and Aerospace Research Laboratories (U.S.) (page images at HathiTrust)
1987 annual report to the Air Force Office of Scientific Research on research on flow control. (Bolling Air Force Base, D. C. : Air Force Office of Scientific Research, United States Air Force, 1987., 1987), by William C. Reynolds, United States. Air Force. Office of Scientific Research, and Stanford University. Department of Mechanical Engineering (page images at HathiTrust)
Management and control of unsteady and turbulent flows (Bolling Air Force Base, D. C. : Air Force Office of Scientific Research, United States Air Force, 1988., 1988), by Hassan M. Nagib, David R. Williams, John L. Way, Candace E. Wark, Patrick H. Reisenthel, Thomas C. Corke, Mukund Acharya, Illinois Institute of Technology. Department of Mechanical and Aerospace Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
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), by L. A. Marshall, United States. Air Force. Systems Command, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Studies in non-linear unsteady aerodynamics (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1988., 1988), by James C. Wu, Georgia Institute of Technology. School of Aerospace Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
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), by E. Albano, L. V. Andrew, United States. Air Force. Systems Command, 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)

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