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  • Automated testing experience of the linear aerospike SR-71 experiment (LASRE) controller [microform] / Richard R. Larson.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Estimated benefits of variable-geometry wing camber control for transport aircraft [microform] / Alexander Bolonkin, Glenn B. Gilyard.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • 1996 NASA-ASEE-Stanford Summer Faculty Fellowship Program [microform] : administrative & summary technical reports : NASA Ames Research Center, grant no. NGT 2-52212 / Ames Research Center, Dryden Flight Research Center, Stanford University.

    • Text
    • [Washington, DC] : Dept. of Aeronautics and Astronautics, Stanford University ; [Springfield, Va. : National Technical Information Service, distributor, 1996-
    • 1996-present

  • High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test [microform] / Brent R. Cobleigh.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
    • 1994

  • Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model [microform] / Stacey J. Cotton and Lisa J. Bjarke.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • In-flight demonstration of a Real-Time Flush Airdata Sensing (RT-FADS) system [microform] / Stephen A. Whitmore, Roy J. Davis, and John Michael Fife.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor], 1995.
    • 1995

  • Comparative optical measurements of airspeed and aerosols on a DC-8 aircraft [microform] / Rodney Bogue ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Drysden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Performance of an electro-hydrostatic actuator on the F-18 systems research aircraft [microform] / Robert Navarro.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • The X-33 extended flight test range [microform] / Dale A. Mackall, Robert Sakahara, Steven E. Kremer.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Forebody flow visualization on the F-18 HARV with actuated forebody strakes [microform] / David F. Fisher and Daniel G. Murri.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • Determination of sun angles for observations of shock waves on a transport aircraft [microform] / David F. Fisher ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • A conversion of wheatstone bridge to current-loop signal conditioning for strain gages [microform] / Karl F. Anderson.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor], 1995.
    • 1995

  • Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivates [microform] / Kenneth W. Iliff, Kon-Sheng Charles Wang.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Reynolds number effects at high angles of attack [microform] / David F. Fisher ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • Conversion from engineering units to telemetry counts on Dryden Flight simulators [microform] / Jay A. Fantini.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • Web-based instruction and learning [microform] : analysis and needs assessment / Barbara Grabowski, Marianne McCarthy, Tiffany Koszalka.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • Anomalous buckling characteristics of laminated metal-matrix composite plates with central square holes [microform] / William L. Ko.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program [microform] / Alexander S. Roudakov and Vyacheslav L. Semenov, John W. Hicks.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft [microform] / W.G. Steenken ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • The use of a lidar forward-looking turbulence sensor for mixed-compression inlet unstart avoidance and gross weight reduction on a high speed civil transport [microform] / David Soreide, Rodney K. Bogue, Jonathan Seidel.

    • Text
    • [Edwards, Calif.] : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Simulator evaluation of simplified propulsion-only emergency flight control systems on transport aircraft [microform] / Frank W. Burcham ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Thermal modeling and analysis of a cryogenic tank design exposed to extreme heating profiles [microform] / Craig A. Stephens, Gregory J. Hanna.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor], 1991.
    • 1991

  • Unsteady aerodynamics [microform] : subsonic compressible inviscid case / A.V. Balakrishman.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Reconfigurable flight control designs with application to the X-33 vehicle [microform] / John J. Burken, Ping Lu, Zhenglu Wu.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Initial flight test of the production support flight control computers at NASA Dryden Flight Research Center [microform] / John Carter, Mark Stephenson.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Airdata measurement and calibration [microform] / Edward A. Haering, Jr.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor], 1995.
    • 1995

  • Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment [microform] / Laurie A. Marshall.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Hanover, MD : NASA Center for AeroSpace Information [distributor] ; Springfield, VA : National Technical Information Service [distributor, 1999]
    • 1999

  • Real-time method for estimating viscous forebody drag coefficients [microform] / Stephen A. Whitemore ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Hanover, MD : NASA Center for AeroSpace Information [distributor] ; Springfield, Va. : National Technical Information Service [distributor, 2000]
    • 2000

  • Design and evaluation of a new boundary-layer rake for flight testing [microform] / Trong T. Bui and David L. Oates, Jose C. Gonsalez.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Hanover, MD : NASA Center for AeroSpace Information [distributor] ; Springfield, VA : National Technical Information Service [distributor, 2000]
    • 2000

  • Pegasus wing-glove experiment to document hypersonic crossflow transition [microform] : measurement system and selected flight results / Arild Bertelrud ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Hanover, MD : NASA Center for AeroSpace Information [distributor] ; Springfield, Va. : National Technical Information Service [distributor, 2000]
    • 2000

  • Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness [microform] / Stephen A. Whitmore, Stephanie Sprague and Johnathan W. Naughton.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [2001]
    • 2001

  • 1984 technical report NASA/ASEE Summer Faculty Fellowship Research Program [microform] : Stanford-Ames-Dryden FRF.

    • Text
    • [Stanford, Calif.] : Dept. of Aeronautics and Astronautics, Stanford University, [1984]
    • 1984

  • High-temperature modal survey of a hot-structure control surface / Natalie D. Spivey.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24035

  • Unsteady aerodynamic model tuning for precise flutter prediction / Chan-gi Pak.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24034

  • Basis function approximation of transonic aerodynamic influence coefficient matrix / Wesley W. Li and Chan-gi Pak.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24037

  • Data driven model development for the supersonic semispan transport (S⁴T) / Sunil L. Kukreja.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24465

  • Flight test results from the rake airflow gage experiment on the F-15B airplane / Michael A. Frederick and Nalin A. Ratnayake.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo30629

  • Flight test of a propulsion-based emergency control system on the MD-11 airplane with emphasis on the lateral axis / John J. Burken [and five others].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, July 1996.
    • 1996-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65384

  • Titanium honeycomb panel testing / W. Lance Richards, Randolph C. Thompson.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, October 1996.
    • 1996-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65662

  • Thermostructural behavior of a hypersonic aircraft sandwich panel subjected to heating on one side / William L. Ko.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, April 1997.
    • 1997-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65665

  • Thrust vectoring on the NASA F-18 high alpha research vehicle / Albion H. Bowers and Joseph W. Pahle.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, November 1996.
    • 1996-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65671

  • High-Alpha handling qualities flight research on the NASA F/A-18 High Alpha Research Vehicle / Keith D. Wichman [and six others]

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, November 1996.
    • 1996-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65674

  • Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV / David F. Fisher, Daniel G. Murri, and Wendy R. Lanser.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, October 1996.
    • 1996-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65675

  • Development of a closed-loop strap down attitude system for an ultrahigh altitude flight experiment / Stephen A. Whitmore, Mike Fife, Logan Brashear.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, January 1997.
    • 1997-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65676

  • Important factors in the maximum likelihood analysis of flight test maneuvers / Kenneth W. Iliff, Richard E. Maine, and T.D. Montgomery.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Office, April 1979.
    • 1979-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70963

  • User's manual for MMLE3, a general FORTRAN program for maximum likelihood parameter estimation / Richard E. Maine and Kenneth W. Iliff.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980.
    • 1980-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70968

  • In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0 / Robert D. Quinn and Leslie Gong.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November1980.
    • 1980-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71370

  • Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane / Frank J. Kurtenbach and Frank W. Burcham, Jr.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, January 1981.
    • 1981-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71438

  • An impact-location estimation algorithm for subsonic uninhabited aircraft / Jeffrey E. Bauer, Edward Teets.

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, November 1997.
    • 1997-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo78986

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