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Airplanes -- Computer simulation

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• Airplanes
• Airplanes -- Mathematical models
• Computer simulation

• Aerodynamics -- Computer simulation
• Aircraft exhaust emissions -- Computer simulation
• Airframes -- Computer simulation
• Airplanes, Military -- Computer simulation
• Flaps (Airplanes) -- Computer simulation
• Hypersonic planes -- Computer simulation
• Pitching (Aerodynamics) -- Computer simulation
• Private flying -- Computer simulation
• Private planes -- Computer simulation
• Propellers, Aerial -- Computer simulation
• Research aircraft -- Computer simulation
• Short take-off and landing aircraft -- Computer simulation
• Spin (Aerodynamics) -- Computer simulation
• Stability of airplanes -- Computer simulation
• Stability of airplanes, Lateral -- Computer simulation
• Stability of airplanes, Longitudinal -- Computer simulation
• Stalling (Aerodynamics) -- Computer simulation
• Supersonic planes -- Computer simulation
• Tailless airplanes -- Computer simulation
• Transport planes -- Computer simulation
• Vibration (Aeronautics) -- Computer simulation
• Airplanes -- Brakes -- Computer simulation
• Airplanes -- Control surfaces -- Computer simulation
• Airplanes -- Control systems -- Computer simulation
• Airplanes -- Fuselage -- Computer simulation
• Airplanes -- Handling characteristics -- Computer simulation
• Airplanes -- Hydraulic equipment -- Computer simulation
• Airplanes -- Jet propulsion -- Computer simulation
• Airplanes -- Landing -- Computer simulation
• Airplanes -- Landing gear -- Computer simulation
• Airplanes -- Motors -- Cowlings -- Materials -- Thermal properties -- Computer simulation
• Airplanes -- Motors -- Thrust -- Computer simulation
• Airplanes -- Motors -- Valves -- Computer simulation
• Airplanes -- Nacelles -- Computer simulation
• Airplanes -- Performance -- Computer simulation
• Airplanes -- Piloting -- Computer simulation
• Airplanes -- Tail surfaces -- Aerodynamics -- Computer simulation
• Airplanes -- Takeoff -- Computer simulation
• Airplanes -- Tires -- Computer simulation
• Airplanes -- Turbofan engines -- Computer simulation
• Airplanes -- Turbojet engines -- Computer simulation
• Airplanes -- Wings -- Computer simulation
• Airplanes -- Wings, Canard -- Aerodynamics -- Computer simulation
• Airplanes -- Wings, Triangular -- Computer simulation

• User's manual for LINEAR, a FORTRAN program to derive linear aircraft models (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), by Eugene L. Duke, Robert F. Antoniewicz, Brian P. Patterson, and Dryden Flight Research Facility (page images at HathiTrust)
• Elements of simulation error analysis (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), by Richard F. Whitbeck, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Inc Systems Technology (page images at HathiTrust)

• 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)

• Effects of jet exhaust gas properties on exhaust simulation and afterbody drag (National Aeronautics and Space Administration ;, 1975), by William B. Compton and Langley Research Center (page images at HathiTrust)
• An analytical study of the effects of jets located more than one jet diameter above a wing at subsonic speeds (National Aeronautics and Space Administration ;, 1974), by Lawrence E. Putnam and Langley Research Center (page images at HathiTrust)

• Development and applications of two computational procedures for determining the vibration modes of structural systems (National Aeronautics and Space Administration ;, 1975), by Raymond G. Kvaternik and Langley Research Center (page images at HathiTrust)

• Air vehicle technology modeling and simulation (Wright Patterson Air Force Base, Ohio : Air Vehicles Directorte, Air Force Research Laboratory, Air Force Materiel Command, 1998., 1988), by Adel Chemaly, Purdue University. School of Aeronautics and Astronautics, and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)

• A computer program to calculate the longitudinal aerodynamic characteristics of wing-flap configurations with extremely blown flaps (National Aeronautics and Space Administration ;, 1976), by M. R. Mendenhall, Selden B. Spangler, Frederick K. Goodwin, Langley Research Center, and Nielsen Engineering & Research (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)

• 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)
• Dynamic heave-pitch analysis of air cushion landing systems (National Aeronautics and Space Administration ;, 1975), by K. M. Captain, D. N. Wormley, Ashok B. Boghani, Langley Research Center, and Foster-Miller Associates (page images at HathiTrust)
• Effect of symmetrical vortex shedding on the longitudinal aerodynamic characteristics of wing-body-tail combinations (National Aeronautics and Space Administration ;, 1975), by M. R. Mendenhall, Jack Norman Nielsen, Ames Research Center, and Nielsen Engineering & Research (page images at HathiTrust)
• The passage of an infinite swept airfoil through an oblique gust (National Aeronautics and Space Administration ;, 1974), by John J. Adamczyk, Langley Research Center, and United Aircraft Corporation. Research Laboratories (page images at HathiTrust)
• Finite element analysis and computer graphics visualization of flow around pitching and plunging airfoils (National Aeronautics and Space Administration ;, 1973), by Theodore Bratanow, Akin Ecer, Langley Research Center, and University of Wisconsin--Milwaukee (page images at HathiTrust)

• PC Pilot: The Complete Guide to Computer Aviation (1994), by Steve Smith (HTML at flightsimbooks.com)

• Prediction of light aircraft horizontal tail onset flows : a review and analysis (National Aeronautics and Space Administration ;, 1977), by Delbert Clyde Summey, Frederick O. Smetana, North Carolina State University, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Point and path performance of light aircraft : a review and analysis (National Aeronautics and Space Administration ;, 1973), by Frederick O. Smetana, W. Donald Johnson, Delbert C. Summey, Langley Research Center, and North Carolina State University (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)

• 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)

• Calculation of the longitudinal aerodynamic characteristics of STOL aircraft with externally-blown jet-augmented flaps (National Aeronautics and Space Administration ;, 1974), by Marnix F. E. Dillenius, Selden B. Spangler, M. R. Mendenhall, Ames Research Center, and Nielsen Engineering & Research (page images at HathiTrust)
• A computer program to calculate the longitudinal aerodynamic characteristics of wing-flap configurations with extremely blown flaps (National Aeronautics and Space Administration ;, 1976), by M. R. Mendenhall, Selden B. Spangler, Frederick K. Goodwin, Langley Research Center, and Nielsen Engineering & Research (page images at HathiTrust)

• Optimal and suboptimal control technique for aircraft spin recovery (National Aeronautics and Space Administration ;, 1974), by John W. Young and Langley Research Center (page images at HathiTrust)

• Stability and control of maneuvering high-performance aircraft (National Aeronautics and Space Administration ;, 1977), by Robert F. Stengel, Paul W. Berry, Analytic Sciences Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A procedure for estimating stability and control parameters from flight test data by using maximum likelihood methods employing a real-time digital system (National Aeronautics and Space Administration ;, 1972), by Randall D. Grove and Langley Research Center (page images at HathiTrust)

• Computed lateral power spectral density response of conventional and STOL airplanes to random atmospheric turbulence (National Aeronautics and Space Administration ;, 1974), by Jacob H. Lichtenstein and Langley Research Center (page images at HathiTrust)

• A parametric study of planform and aeroelastic effects on aerodynamic center, [alpha]- and q-stability derivatives : summary report (National Aeronautics and Space Administration ;, 1973), by Jan Roskam, C. Edward Lan, Langley Research Center, and University of Kansas (page images at HathiTrust)
• Effect of symmetrical vortex shedding on the longitudinal aerodynamic characteristics of wing-body-tail combinations (National Aeronautics and Space Administration ;, 1975), by M. R. Mendenhall, Jack Norman Nielsen, Ames Research Center, and Nielsen Engineering & Research (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)
• Analysis of helicopter rotor blade torsional oscillations due to stall (National Aeronautics and Space Administration ;, 1975), by Peter Crimi, U.S. Army Air Mobility Research and Development Laboratory, Langley Research Center, and Avco Corporation. Systems Division (page images at HathiTrust)
• Investigation of nonlinear inviscid and viscous flow effects in the analysis of dynamic stall (National Aeronautics and Space Administration ;, 1974), by Peter Crimi, Langley Research Center, and Avco Corporation. Systems Division (page images at HathiTrust)
• A design summary of stall characteristics of straight wing aircraft (National Aeronautics and Space Administration ;, 1971), by M. A. McVeigh, E. Kisielowski, United States National Aeronautics and Space Administration, Langley Research Center, and Dynasciences Corporation. Scientific Systems Division (page images at HathiTrust)
• Analysis of stall flutter of a helicopter rotor blade (National Aeronautics and Space Administration ;, 1973), by Peter Crimi, Langley Research Center, and Avco Corporation. Systems Division (page images at HathiTrust)

• Aerodynamic design and analysis system for supersonic aircraft (National Aeronautics and Space Administration ;, 1975), by W. D. Middleton, R. G. Coleman, J. L. Lundry, Langley Research Center, and Boeing Commercial Airplane 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)

• Preliminary performance estimates of an oblique, all-wing, remotely piloted vehicle for air-to-air combat (National Aeronautics and Space Administration ;, 1974), by Walter P. Nelms, Rodney O. Bailey, and Ames Research Center (page images at HathiTrust)

• Aircraft design for mission performance using nonlinear multiobjective optimization methods (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division :, 1990), by Augustine R. Dovi, Gregory A. Wrenn, and Langley Research Center (page images at HathiTrust)

• Analysis of helicopter rotor blade torsional oscillations due to stall (National Aeronautics and Space Administration ;, 1975), by Peter Crimi, U.S. Army Air Mobility Research and Development Laboratory, Langley Research Center, and Avco Corporation. Systems Division (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)
• A study of the dynamics of airplane braking systems as affected by tire elasticity and brake response (National Aeronautics and Space Administration ;, 1965), by Sidney A. Batterson and Langley Research Center (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)
• 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)

• A controls engineering approach for analyzing airplane input-output characteristics (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by P. Douglas Arbuckle and Langley Research Center (page images at HathiTrust)
• 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)
• A method to stabilize linear systems using Eigenvalue gradient information (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Carol D. Wieseman and Langley Research Center (page images at HathiTrust)
• A knowledge-based system design/information tool (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by James G. Allen, Scott E. Sikora, Dryden Flight Research Facility, and Charles Stark Draper Laboratory (page images at HathiTrust)
• Stability and control of maneuvering high-performance aircraft (National Aeronautics and Space Administration ;, 1977), by Robert F. Stengel, Paul W. Berry, Analytic Sciences Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A mathematical model of an active control landing gear for load control during impact and roll-out (National Aeronautics and Space Administration ;, 1976), by John R. McGehee, Huey D. Carden, and Langley Research Center (page images at HathiTrust)
• A procedure for estimating stability and control parameters from flight test data by using maximum likelihood methods employing a real-time digital system (National Aeronautics and Space Administration ;, 1972), by Randall D. Grove and Langley Research Center (page images at HathiTrust)
• Optimal and suboptimal control technique for aircraft spin recovery (National Aeronautics and Space Administration ;, 1974), by John W. Young and Langley Research Center (page images at HathiTrust)

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