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Aerodynamics -- Computer simulation

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• Aerodynamics
• Dynamics -- Computer simulation
• Gas dynamics -- Computer simulation
• Airplanes -- Computer simulation
• Aerodynamics -- Mathematical models
• Computer simulation

• Aerodynamic heating -- Computer simulation
• Aerodynamic load -- Computer simulation
• Aerodynamics, Hypersonic -- Computer simulation
• Aerodynamics, Supersonic -- Computer simulation
• Aerodynamics, Transonic -- Computer simulation
• Aeroelasticity -- Computer simulation
• Angle of attack (Aerodynamics) -- Computer simulation
• Body of revolution -- Computer simulation
• Boundary layer -- Computer simulation
• Cascades (Fluid dynamics) -- Computer simulation
• Downwash (Aerodynamics) -- Computer simulation
• Drag (Aerodynamics) -- Computer simulation
• Flutter (Aerodynamics) -- Computer simulation
• Gas flow -- Computer simulation
• Ground-cushion phenomenon -- Computer simulation
• Interference (Aerodynamics) -- Computer simulation
• Leading edges (Aerodynamics) -- Computer simulation
• Lift (Aerodynamics) -- Computer simulation
• Pitching (Aerodynamics) -- Computer simulation
• Spin (Aerodynamics) -- Computer simulation
• Stability of airplanes -- Computer simulation
• Stalling (Aerodynamics) -- Computer simulation
• Stratified flow -- Computer simulation
• Trajectory optimization -- Computer simulation
• Unsteady flow (Aerodynamics) -- Computer simulation
• Vortex-motion -- Computer simulation
• Wakes (Aerodynamics) -- Computer simulation
• Aerofoils -- Aerodynamics -- Computer simulation
• Air ducts -- Aerodynamics -- Computer simulation
• Airplanes -- Tail surfaces -- Aerodynamics -- Computer simulation
• Airplanes -- Wings, Canard -- Aerodynamics -- Computer simulation
• Compressors -- Aerodynamics -- Computer simulation
• Cone -- Aerodynamics -- Computer simulation
• Diffusers -- Aerodynamics -- Computer simulation
• Flaps (Airplanes) -- Aerodynamics -- Computer simulation
• Gas-turbines -- Aerodynamics -- Computer simulation
• Guided missiles -- Aerodynamics -- Computer simulation
• Helicopters -- Aerodynamics -- Computer simulation
• Jet planes -- Aerodynamics -- Computer simulation
• Mars probes -- Aerodynamics -- Computer simulation
• Parachutes -- Aerodynamics -- Computer simulation
• Rockets (Aeronautics) -- Aerodynamics -- Computer simulation
• Rotors (Helicopters) -- Aerodynamics -- Computer simulation
• Short take-off and landing aircraft -- Aerodynamics -- Computer simulation
• Space shuttles -- Aerodynamics -- Computer simulation
• Space vehicles -- Aerodynamics -- Computer simulation
• Turbines -- Aerodynamics -- Computer simulation
• Turbomachines -- Aerodynamics -- Computer simulation

• Linearized aerodynamic and control law models of the X-29A airplane and comparison with flight data (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by John T. Bosworth and Dryden Flight Research Facility (page images at HathiTrust)
• Semianalytic modeling of aerodynamic shapes (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Raymond L. Barger, Mary S. Adams, and Langley Research Center (page images at HathiTrust)
• An improved method for the aerodynamic analysis of wing-body-tail configurations in subsonic and supersonic flow (National Aeronautics and Space Administration ;, 1973), by F. A. Woodward, Langley Research Center, and Aerophysics Research Corporation (page images at HathiTrust)
• Subsonic panel method for the efficient analysis of multiple geometry perturbations (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1982), by D. R. Bristow, J. Dennis Hawk, Langley Research Center, and McDonnell Aircraft Company (page images at HathiTrust)
• Computed lateral rate and acceleration power spectral response of conventional and STOL airplanes to atmospheric turbulence (National Aeronautics and Space Administration ;, 1975), by Jacob H. Lichtenstein and Langley Research Center (page images at HathiTrust)
• Development and application of a local linearization algorithm for the integration of quaternion rate equations in real-time flight simulation problems (National Aeronautics and Space Administration ;, 1973), by Lawrence E. Barker, Louise H. Williams, Roland L. Bowles, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Subsonic annular wing theory with application to flow about nacelles (National Aeronautics and Space Administration ;, 1974), by Michael J. Mann and Langley Research Center (page images at HathiTrust)
• A rapid numerical solution to subsonic flow over planar and axisymmetric profiles at an angle of attack of 0 ̊ (National Aeronautics and Space Administration ;, 1974), by Vincent R. Mascitti and Langley Research Center (page images at HathiTrust)

• A simplified method for thermal analysis of a cowl leading edge subject to intense local shock-wave-interference heating (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by David M. McGowan, Stephen J. Scotti, Charles J. Camarda, and Langley Research Center (page images at HathiTrust)
• Analysis of various descent trajectories for a hypersonic-cruise, cold-wall research airplane (National Aeronautics and Space Administration ;, 1975), by Pierce L. Lawing and Langley Research Center (page images at HathiTrust)
• Numerical computation of aerodynamic heating of liquid propellants (National Aeronautics and Space Administration, 1960), by John L. Kramer, William H. Roudebush, Herman H. Lowell, and Lewis Research Center (page images at HathiTrust)
• A new technique for calculating reentry base heating (National Aeronautics and Space Administration ;, 1973), by James C. S. Meng and George C. Marshall Space Flight Center. Aero-Astrodynamics Laboratory (page images at HathiTrust)

• Steady and unsteady aerodynamic forces from the SOUSSA surface-panel method for a fighter wing with tip missile and comparison with experiment and PANAIR (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by Herbert J. Cunningham and Langley Research Center (page images at HathiTrust)
• Comparison of theoretical and experimental steady wing loads on a space shuttle configuration at Mach numbers of 0.6 and 1.4 (National Aeronautics and Space Administration ;, 1976), by John S. Preisser, Harold E. Lowder, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Prediction of span loading of straight-wing/propeller combinations up to stall (National Aeronautics and Space Administration ;, 1975), by M. A. McVeigh, E. Kisielowski, L. Gray, Lanlgley Research Center, and Inc United Technology (page images at HathiTrust)
• Prediction of unsteady aerodynamic loadings caused by leading edge and trailing edge control surface motions in subsonic compressible flow : analysis and results (National Aeronautics and Space Administration ;, 1975), by W. S. Rowe, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• The effect of helicopter main rotor blade phasing and spacing on performance, blade loads, and acoustics (National Aeronautics and Space Administration ;, 1976), by Santu T. Gangwani, Systems Research Laboratories. Rasa Division, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Numerical calculations of velocity and pressure distribution around oscillating airfoils (National Aeronautics and Space Administration ;, 1974), by Theodore Bratanow, Michael Kobiske, Akin Ecer, Langley Research Center, and University of Wisconsin--Milwaukee (page images at HathiTrust)
• Prediction of unsteady aerodynamic loadings caused by trailing edge control surface motions in subsonic compressible flow : analysis and results (National Aeronautics and Space Administration ;, 1972), by W. S. Rowe, M. C. Redman, B. A. Winther, Langley Research Center, and Boeing Company (page images at HathiTrust)
• Analytical method for predicting the pressure distribution about a nacelle at transonic speeds (National Aeronautics and Space Administration ;, 1973), by J. S. Keith, Langley Research Center, and General Electric Company (page images at HathiTrust)
• Subsonic panel method for the efficient analysis of multiple geometry perturbations (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1982), by D. R. Bristow, J. Dennis Hawk, Langley Research Center, and McDonnell Aircraft Company (page images at HathiTrust)
• Combined linear theory/impact theory for analysis and design of high speed configurations (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980), by D. Brooke, Langley Research Center, McDonnell Aircraft Company, and D. V. Vondrasek (page images at HathiTrust)
• A modified Theodorsen [epsilon]-function airfoil design procedure (National Aeronautics and Space Administration ;, 1974), by Raymond L. Barger and Langley Research Center (page images at HathiTrust)
• Subsonic annular wing theory with application to flow about nacelles (National Aeronautics and Space Administration ;, 1974), by Michael J. Mann and Langley Research Center (page images at HathiTrust)
• Boundary-layer transition and displacement-thickness effects on zero-lift drag of a series of power-law bodies at Mach 6 (National Aeronautics and Space Administration ;, 1974), by George C. Ashby, Julius E. Harris, and Langley Research Center (page images at HathiTrust)

• A simplified method for thermal analysis of a cowl leading edge subject to intense local shock-wave-interference heating (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by David M. McGowan, Stephen J. Scotti, Charles J. Camarda, and Langley Research Center (page images at HathiTrust)
• An upwind-biased space marching algorithm for supersonic viscous flow (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by Francis A. Greene and Langley Research Center (page images at HathiTrust)
• Improved tangent-cone method for the Aerodynamic Preliminary Analysis System (APAS) version of the Hypersonic Arbitrary-Body Program (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Christopher I. Cruz, Gregory J. Sova, and Langley Research Center (page images at HathiTrust)
• Hypersonic ionizing air viscous shock-layer flows over nonanalytic blunt bodies (National Aeronautics and Space Administration ;, 1975), by Miner. E. W. (Earnest Wade), Clark H. Lewis, Lyndon B. Johnson Space Center, and Virginia Polytechnic Institute and State University. Aerospace and Ocean Engineering Dept (page images at HathiTrust)
• Hypersonic aerodynamic characteristics of a family of power-law, wing-body configuratioons (National Aeronautics and Space Administration ;, 1973), by James C. Townsend and Langley Research Center (page images at HathiTrust)
• Boundary-layer transition and displacement-thickness effects on zero-lift drag of a series of power-law bodies at Mach 6 (National Aeronautics and Space Administration ;, 1974), by George C. Ashby, Julius E. Harris, and Langley Research Center (page images at HathiTrust)
• Mark IV supersonic-hypsersonic arbitrary-body program modifications and computer graphics. Volume II, Computer graphics (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), by S. Taylor, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, and inc Science Applications (page images at HathiTrust)
• Mark IV supersonic-hypsersonic arbitrary-body program modifications and computer graphics. Volume I, Surface streamline tracing (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), by S. Taylor, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, and inc Science Applications (page images at HathiTrust)

• Fuselage design for a specified Mach-sliced area distribution (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Raymond L. Barger, Mary S. Adams, and Langley Research Center (page images at HathiTrust)
• Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings : a correlation with experiment (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by S. Naomi McMillin, Earll M. Murman, James L. Thomas, and Langley Research Center (page images at HathiTrust)
• Equilibrium chemical reaction of supersonic hydrogen-air jets : the Alma computer program (National Aeronautics and Space Administration ;, 1977), by S. Elghobashi, D. B. Spalding, Fluid Mechanics and Thermal Systems, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Combustion of hydrogen injected into a supersonic airstream (the ship computer program) (National Aeronautics and Space Administration ;, 1977), by N. C. Markatos, D. G. Tatchell, D. B. Spalding, Fluid Mechanics and Thermal Systems, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The effects of winglets on low aspect ratio wings at supersonic Mach numbers (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), by James A. Keenan, John Kuhlman, Langley Research Center, and West Virginia University. Dept. of Mechanical and Aerospace Engineering (page images at HathiTrust)
• NASA TN D-5537 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Vincent R. Mascitti, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Assessment of an analytical procedure for predicting supersonic ejector nozzle performance (National Aeronautics and Space Administration ;, 1974), by Bernhard H. Anderson and Lewis Research Center (page images at HathiTrust)
• Mark IV supersonic-hypsersonic arbitrary-body program modifications and computer graphics. Volume II, Computer graphics (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), by S. Taylor, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, and inc Science Applications (page images at HathiTrust)
• Mark IV supersonic-hypsersonic arbitrary-body program modifications and computer graphics. Volume I, Surface streamline tracing (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), by S. Taylor, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, and inc Science Applications (page images at HathiTrust)

• Relative efficiency and accuracy of two Navier-Stokes codes for simulating attached transonic flow over wings (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by Daryl L. Bonhaus, Stephen F. Wornom, and Langley Research Center (page images at HathiTrust)
• Prediction of effects of wing contour modifications on low-speed maximum lift and transonic performance for the EA-6B aircraft (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Dennis O. Allison, E. G. Waggoner, and Langley Research Center (page images at HathiTrust)
• Calculation of unsteady transonic flows with mild separation by viscous-inviscid interaction (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by James T. Howlett and Langley Research Center (page images at HathiTrust)
• Computation of the transonic perturbation flow fields around two- and three-dimensional oscillating wings (National Aeronautics and Space Administration ;, 1975), by W. H. Weatherill, James D. Sebastian, F. Edward Ehlers, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Computation of unsteady transonic flows through rotating and stationary cascades. (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by John I. Erdos, Lewis Research Center, and Advanced Technology Laboratories (page images at HathiTrust)
• Calculative techniques for transonic flows about certain classes of wing-body combinations (National Aeronautics and Space Administration ;, 1972), by Stephen S. Stahara, John R. Spreiter, Ames Research Center, and Nielsen Engineering & Research (page images at HathiTrust)
• High-speed flow past wings (National Aeronautics and Space Administration ;, 1973), by Helge Nørstrud, Langley Research Center, and Lockheed-Georgia Company (page images at HathiTrust)
• Analysis of a theoretically optimized transonic airfoil (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by M. E. Lores, George D. Shrewsbury, Kenneth P. Burdges, Ames Research Center, and Lockheed-Georgia Company (page images at HathiTrust)
• A finite difference method for the solution of the transonic flow around harmonically oscillating wings (National Aeronautics and Space Administration ;, 1974), by F. Edward Ehlers, Langley Research Center, and Boeing Commercial Airplane Company (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)
• Numerical calculations of two-dimensional, unsteady transonic flows with circulation (National Aeronautics and Space Administration ;, 1974), by Richard M. Beam, Robert F. Warming, and Ames Research Center (page images at HathiTrust)
• An analysis method for two-dimensional transonic viscous flow (National Aeronautics and Space Administration ;, 1975), by Paul C. Bavitz and Langley Research Center (page images at HathiTrust)

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