Gas dynamics -- Computer simulation

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• Gas dynamics
• Fluid dynamics -- Computer simulation
• Gas dynamics -- Mathematical models
• Computer simulation

• Aerodynamics -- Computer simulation
• Gas flow -- Computer simulation

• Graphical results for large-amplitude unsteady one-dimensional waves in magnetized collision-free plasmas with discrete structure / by Wm. Prichard Jones and Vernon J. Rossow. (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1965]), by W. P. Jones (page images at HathiTrust)

• Linearized aerodynamic and control law models of the X-29A airplane and comparison with flight data / John T. Bosworth. (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by John T. Bosworth (page images at HathiTrust)
• Semianalytic modeling of aerodynamic shapes / Raymond L. Barger and Mary S. Adams. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by Raymond L. Barger (page images at HathiTrust)
• Subsonic panel method for the efficient analysis of multiple geometry perturbations / D.R. Bristow and J.D. Hawk. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1982), by D. R. Bristow (page images at HathiTrust)

• A simplified method for thermal analysis of a cowl leading edge subject to intense local shock-wave-interference heating / David M. McGowan, Charles J. Camarda, and Stephen J. Scotti. (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by David M. McGowan (page images at HathiTrust)
• Numerical computation of aerodynamic heating of liquid propellants / by John L. Kramer, Herman H. Lowell and William H. Roudebush. (Washington : National Aeronautics and Space Administration, [1960]), by John L. Kramer (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 / Herbert J. Cunningham. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Herbert J. Cunningham (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 / John S. Preisser and Harold E. Lowder, Jr. (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by John S. Preisser (page images at HathiTrust)
• Prediction of span loading of straight-wing/propeller combinations up to stall / M.A. McVeigh, L. Gray, and E. Kisielowski. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by M. A. McVeigh (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 / W.S. Rowe ... [et al.]. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]) (page images at HathiTrust)
• The effect of helicopter main rotor blade phasing and spacing on performance, blade loads, and acoustics / Santu T. Gangwani ; prepared by Rochester Applied Science Associates. (Washington : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the National Technical Information Service, 1976), by Santu T. Gangwani (page images at HathiTrust)
• Prediction of unsteady aerodynamic loadings caused by trailing edge control surface motions in subsonic compressible flow : analysis and results / by W.S. Rowe, B.A. Winther, and M.C. Redman. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by W. S. Rowe (page images at HathiTrust)
• Subsonic panel method for the efficient analysis of multiple geometry perturbations / D.R. Bristow and J.D. Hawk. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1982), by D. R. Bristow (page images at HathiTrust)
• Combined linear theory/impact theory for analysis and design of high speed configurations / D. Brooke and D.V. Vondrasek. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980), by D. Brooke (page images at HathiTrust)

• A simplified method for thermal analysis of a cowl leading edge subject to intense local shock-wave-interference heating / David M. McGowan, Charles J. Camarda, and Stephen J. Scotti. (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by David M. McGowan (page images at HathiTrust)
• Improved tangent-cone method for the Aerodynamic Preliminary Analysis System (APAS) version of the Hypersonic Arbitrary-Body Program / Christopher I. Cruz, Gregory J. Sova. (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Christopher I. Cruz (page images at HathiTrust)
• Hypersonic ionizing air viscous shock-layer flows over nonanalytic blunt bodies / E.W. Miner and Clark H. Lewis. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by Miner. E. W. (Earnest Wade) (page images at HathiTrust)

• Fuselage design for a specified Mach-sliced area distribution / Raymond L. Barger and Mary S. Adams. (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Raymond L. Barger (page images at HathiTrust)
• Equilibrium chemical reaction of supersonic hydrogen-air jets : the Alma computer program / S. Elghobashi and D.B. Spalding. (Washington : National Aeronautics and Space Administration ; Springfield, Va. : S. Elghobashi and D.B. Spalding.), by S. Elghobashi (page images at HathiTrust)
• Combustion of hydrogen injected into a supersonic airstream (the ship computer program) / N.C. Markatos, D.B. Spalding and D.G. Tatchell. (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by N. C. Markatos (page images at HathiTrust)
• The effects of winglets on low aspect ratio wings at supersonic Mach numbers / James A. Keenan and John M. Kuhlman. (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by James A. Keenan (page images at HathiTrust)
• An approximate solution of additive-drag coefficient and mass-flow ratio for inlets utilizing right circular cones at zero angle of attack / Vincent R. Mascitti. (Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Vincent R. Mascitti (page images at HathiTrust)

• Computation of the transonic perturbation flow fields around two- and three-dimensional oscillating wings / Warren H. Weatherill, F. Edward Ehlers, and James D. Sebastian. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by W. H. Weatherill (page images at HathiTrust)
• Calculation of unsteady transonic flows with mild separation by viscous-inviscid interaction / James T. Howlett. (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by James T. Howlett (page images at HathiTrust)
• Computation of unsteady transonic flows through rotating and stationary cascades. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977) (page images at HathiTrust)
• Analysis of a theoretically optimized transonic airfoil / M.E. Lores, K.P. Burdges, and G.d. Shrewsbury. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by M. E. Lores (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 / Herbert J. Cunningham. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Herbert J. Cunningham (page images at HathiTrust)
• Analysis of helicopter rotor blade torsional oscillations due to stall / Peter Crimi. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Peter Crimi (page images at HathiTrust)

• Angle-of-attack analysis for Project Fire 1 payload reentry flight / by Gerard E. Woodbury. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1966]), by Gerard E. Woodbury (page images at HathiTrust)

• Semianalytic modeling of aerodynamic shapes / Raymond L. Barger and Mary S. Adams. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by Raymond L. Barger (page images at HathiTrust)
• Transient response of shells of revolution by direct integration and modal superposition methods / by Wendell B. Stephens and Howard M. Adelman. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by Wendell B. Stephens (page images at HathiTrust)

• Direct simulation of high-speed mixing layers / H.S. Mukunda ... [et al.]. (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992) (page images at HathiTrust)
• Modeling of the heat transfer in bypass transitional boundary-layer flows / Frederick F. Simon, Craig A. Stephens. (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by Frederick F. Simon (page images at HathiTrust)
• Testing of transition-region models, test cases and data Bart A. Singer, Surya P.G. Dinavahi, Venkit Iyer. ([Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]), by Bart A. Singer (page images at HathiTrust)
• Inverse solutions for laminar boundary-layer flows with separation and reattachment / James E. Carter. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by James E. Carter (page images at HathiTrust)

• Computation of unsteady transonic flows through rotating and stationary cascades. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977) (page images at HathiTrust)

• Prediction of light aircraft horizontal tail onset flows : a review and analysis / Delbert C. Summey and Frederick O. Smetana. (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Delbert Clyde Summey (page images at HathiTrust)

• Improved tangent-cone method for the Aerodynamic Preliminary Analysis System (APAS) version of the Hypersonic Arbitrary-Body Program / Christopher I. Cruz, Gregory J. Sova. (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Christopher I. Cruz (page images at HathiTrust)
• The effects of winglets on low aspect ratio wings at supersonic Mach numbers / James A. Keenan and John M. Kuhlman. (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by James A. Keenan (page images at HathiTrust)
• Combined linear theory/impact theory for analysis and design of high speed configurations / D. Brooke and D.V. Vondrasek. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980), by D. Brooke (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 / Herbert J. Cunningham. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Herbert J. Cunningham (page images at HathiTrust)
• A method to stabilize linear systems using Eigenvalue gradient information / Carol D. Wieseman. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by Carol D. Wieseman (page images at HathiTrust)
• Computer program for supersonic kernel-function flutter analysis of thin lifting surfaces / by Herbert J. Cunningham. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Herbert J. Cunningham (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 / W.S. Rowe ... [et al.]. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]) (page images at HathiTrust)
• Prediction of unsteady aerodynamic loadings caused by trailing edge control surface motions in subsonic compressible flow : analysis and results / by W.S. Rowe, B.A. Winther, and M.C. Redman. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by W. S. Rowe (page images at HathiTrust)
• Analysis of stall flutter of a helicopter rotor blade / by Peter Crimi. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Peter Crimi (page images at HathiTrust)

• Combustion of hydrogen injected into a supersonic airstream (the ship computer program) / N.C. Markatos, D.B. Spalding and D.G. Tatchell. (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by N. C. Markatos (page images at HathiTrust)
• Real-gas effects in critical-flow-through nozzles and tabulated thermodynamic properties / by Robert C. Johnson. (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1965]), by Robert C. Johnson (page images at HathiTrust)

• Dynamic heave-pitch analysis of air cushion landing systems / K.M. Captain, A.B. Boghani, and D.N. Wormley. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by K. M. Captain (page images at HathiTrust)

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