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Dryden Flight Research Facility

Books from the extended shelves:

Dryden Flight Research Facility: Aerothermal test results from the first flight of the Pegasus air-launched space booster (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by Gregory Noffz (page images at HathiTrust)
Dryden Flight Research Facility: Aircraft flight test trajectory control (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by P. K. A. Menon and R. A. Walker (page images at HathiTrust)
Dryden Flight Research Facility: Aircraft ground tests and subscale model results of axial thrust loss caused by thrust vectoring using turning vanes (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Steven A. Johnson (page images at HathiTrust)
Dryden Flight Research Facility: Application and flight test of linearizing transformations using measurement feedback to the nonlinear control problem (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by Robert F. Antoniewicz, Eugene L. Duke, and P. K. A. Menon (page images at HathiTrust)
Dryden Flight Research Facility: Assessment of flying-quality criteria for air-breathing aerospacecraft (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Duane T. McRuer and inc Systems Technology (page images at HathiTrust)
Dryden Flight Research Facility: Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by William L. Ko and Raymond H. Jackson (page images at HathiTrust)
Dryden Flight Research Facility: Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by William L. Ko and Raymond H. Jackson (page images at HathiTrust)
Dryden Flight Research Facility: Compressive buckling analysis of hat-stiffened panel (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), also by William L. Ko and Raymond H. Jackson (page images at HathiTrust)
Dryden Flight Research Facility: Design considerations of manipulator and feel system characteristics in roll tracking (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by Donald E. Johnston and Bimal L. Aponso (page images at HathiTrust)
Dryden Flight Research Facility: Design of control laws for flutter suppression based on the aerodynamic energy concept and comparisons with other design methods (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by E. Nissim (page images at HathiTrust)
Dryden Flight Research Facility: A design procedure for the handling qualities optimization of the X-29A aircraft (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by John T. Bosworth and Timothy H. Cox (page images at HathiTrust)
Dryden Flight Research Facility: Determination of the effects of heating on modal characteristics of an aluminum plate with application to hypersonic vehicles (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by H. Todd Snyder and M. W. Kehoe (page images at HathiTrust)
Dryden Flight Research Facility: Development of an integrated aeroservoelastic analysis program and correlation with test data (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Kajal K. Gupta, L. S. Voelker, and M. J. Brenner (page images at HathiTrust)
Dryden Flight Research Facility: Effect of control surface mass unbalance on the stability of a closed-loop active control system (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by E. Nissim (page images at HathiTrust)
Dryden Flight Research Facility: The effectiveness of vane-aileron excitation in the experimental determination of flutter speed by parameter identification (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by E. Nissim (page images at HathiTrust)
Dryden Flight Research Facility: Effects of cockpit lateral stick characteristics on handling qualities and pilot dynamics (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by David G. Mitchell, David H. Klyde, Bimal L. Aponso, Inc PRC, and inc Systems Technology (page images at HathiTrust)
Dryden Flight Research Facility: Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Donald L. Hughes, Karen G. Mackall, and Lawrence P. Myers (page images at HathiTrust)
Dryden Flight Research Facility: Evaluation of various thrust calibration [i.e. calculation] techniques on an F404 engine (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Ronald J. Ray (page images at HathiTrust)
Dryden Flight Research Facility: Experimental characterization of the effects of pneumatic tubing on unsteady pressure measurements (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Stephen A. Whitmore (page images at HathiTrust)
Dryden Flight Research Facility: Failure detection and fault management techniques for a pneumatic high-angle-of-attack flush airdata sensing (HI-FADS) system (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Stephen A. Whitmore and Timothy R. Moes (page images at HathiTrust)
Dryden Flight Research Facility: Flight characteristics of a modified Schweizer SGS 1-36 sailplane at low and very high angles of attack (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Alex G. Sim (page images at HathiTrust)
Dryden Flight Research Facility: Flight control system design factors for applying automated testing techniques (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Joel R. Sitz and Todd H. Vernon (page images at HathiTrust)
Dryden Flight Research Facility: Flight-determined benefits of integrated flight-propulsion control systems (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by James F. Stewart, Donald H. Gatlin, and Frank W. Burcham (page images at HathiTrust)
Dryden Flight Research Facility: Flight evaluation of a pneumatic system for unsteady pressure measurements using conventional sensors (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Robert E. Curry and Glenn B. Gilyard (page images at HathiTrust)
Dryden Flight Research Facility: Flight vehicle thermal testing with infrared lamps (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by Roger A. Fields (page images at HathiTrust)
Dryden Flight Research Facility: Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Lawrence C. Freudinger (page images at HathiTrust)
Dryden Flight Research Facility: In-flight flow visualization characteristics of the NASA F-18 high alpha research vehicle at high angles of attack (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by David F. Fisher, David M. Richwine, and John H. Del Frate (page images at HathiTrust)
Dryden Flight Research Facility: An in-flight technique for wind measurement in support of the space shuttle program (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Lisa J. Bjarke and L. J. Ehernberger (page images at HathiTrust)
Dryden Flight Research Facility: In-flight transition measurement on a 10⁰ cone at Mach numbers from 0.5 to 2.0 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by David F. Fisher, N. Sam Dougherty, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Dryden Flight Research Facility: Integrated flight propulsion control research results using the NASA F-15 HIDEC flight research facility (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by James F. Stewart (page images at HathiTrust)
Dryden Flight Research Facility: A knowledge based application of the extended aircraft interrogation and display system (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by Richard D. Glover and Richard R. Larson (page images at HathiTrust)
Dryden Flight Research Facility: A knowledge-based system design/information tool (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by James G. Allen, Scott E. Sikora, and Charles Stark Draper Laboratory (page images at HathiTrust)
Dryden Flight Research Facility: 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), also by John T. Bosworth (page images at HathiTrust)
Dryden Flight Research Facility: Measurement effects on the calculation of in-flight thrust for an F404 turbofan engine (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by Timothy E. Conners (page images at HathiTrust)
Dryden Flight Research Facility: Model authoring system for fail safe analysis (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Scott E. Sikora and Charles Stark Draper Laboratory (page images at HathiTrust)
Dryden Flight Research Facility: Multilayer theory for delamination analysis of a composite curved bar subjected to end forces and end moments (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by William L. Ko and Raymond H. Jackson (page images at HathiTrust)
Dryden Flight Research Facility: Open-mode delamination stress concentrations in horseshoe and elliptic composite curved bars subjected to end forces (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by William L. Ko and Raymond H. Jackson (page images at HathiTrust)
Dryden Flight Research Facility: Optimal cooperative control synthesis of active displays (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987), also by Sanjay Gary and D. K. Schmidt (page images at HathiTrust)
Dryden Flight Research Facility: Optimum element density studies for finite-element thermal analysis of hypersonic aircraft structures (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by William L. Ko, Kyle M. Muramoto, and Timothy Olona (page images at HathiTrust)
Dryden Flight Research Facility: A preliminary evaluation of an F100 engine parameter estimation process using flight data (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Trindel A. Maine, Heather H. Lambert, and Glenn B. Gilyard (page images at HathiTrust)
Dryden Flight Research Facility: Preliminary flight evaluation of an engine performance optimization algorithm (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by Heather H. Lambert (page images at HathiTrust)
Dryden Flight Research Facility: A Preliminary investigation of the use of throttles for emergency flight control (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by Frank W. Burcham (page images at HathiTrust)
Dryden Flight Research Facility: Proceedings of the X-15 First Flight 30th Anniversary Celebration (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), also by Calif.) X-15 First Flight 30th Anniversary Celebration (1989 : Edwards and Kenneth E. Hodge (page images at HathiTrust)
Dryden Flight Research Facility: A proposed Kalman filter algorithm for estimation of unmeasured output variables for an F100 turbofan engine (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Gurbux S. Alag and Glenn B. Gilyard (page images at HathiTrust)
Dryden Flight Research Facility: Propulsion system/flight control integration and optimization : flight evaluation and technology transition (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Frank W. Burcham, Lawrence P. Myers, and Glenn B. Gilyard (page images at HathiTrust)
Dryden Flight Research Facility: Real-time aerodynamic heating and surface temperature calculations for hypersonic flight simulation (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Robert D. Quinn and Leslie Gong (page images at HathiTrust)
Dryden Flight Research Facility: Rule-based air combat simulation (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), also by George H. Burgin and L. B. Sidor (page images at HathiTrust)
Dryden Flight Research Facility: A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Steven A. Johnson (page images at HathiTrust)
Dryden Flight Research Facility: A Simulation evaluation of a four-engine jet transport using engine thrust modulation for flightpath control (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), also by Glenn B. Gilyard (page images at HathiTrust)
Dryden Flight Research Facility: A smoke generator system for aerodynamic flight research (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by David M. Richwine, Gene V. Tracy, and Robert E. Curry (page images at HathiTrust)
Dryden Flight Research Facility: Teaching high-performance skills using above-real-time training (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993), also by Dutch Guckenberger, Norman E. Lane, Kevin C. Uliano, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
Dryden Flight Research Facility: Thermal and structural tests of René 41 honeycomb integral-tank concept for future space transportation systems (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), also by John L. Shideler (page images at HathiTrust)
Dryden Flight Research Facility: User's manual for LINEAR, a FORTRAN program to derive linear aircraft models (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), also by Eugene L. Duke, Robert F. Antoniewicz, and Brian P. Patterson (page images at HathiTrust)
Dryden Flight Research Facility: Variable-camber systems integration and operational performance of the AFTI/F-111 mission adaptive wing (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program , 1992), also by John W. Smith, Gordon A. Payne, and Wilton P. Lock (page images at HathiTrust)

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