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  • Biomechanically induced and controller coupled oscillations experienced on the F-16XL aircraft during rolling maneuvers / John W. Smith and Terry Montgomery.

    • Text
    • Edwards, California : 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/gpo65454

  • Least squares best fit method for the three parameter Weibull distribution : analysis of tensile and bend specimens with volume or surface flaw failure / Bernard Gross.

    • 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/gpo65364

  • Dynamic analysis with stress mode animation by the integrated force method / Surya N. Patnaik, Rula M. Coroneos and Dale A. Hopkins.

    • 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/gpo65374

  • Development and flight test of an augmented thrust-only flight control system on an MD- 11 transport airplane / Frank W. Burcham, Jr. [and three 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/gpo65382

  • 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

  • Structural dynamic model obtained from flight for use with piloted simulation and handling qualities analysis / Bruce G. Powers.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, June 1996.
    • 1996-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65385

  • Probabilistic micromechanics and macromechanics for ceramic matrix composites / Pappu L.N. Murthy, Subodh K. Mital, Ashwin R. Shah.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, June 1997.
    • 1997-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65563

  • 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

  • Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation / William L. Ko.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, December 1996.
    • 1996-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65666

  • 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

  • Performance trend of different algorithms for structural design optimization / Surya N. Patnaik [and three others].

    • 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/gpo65359

  • An overview of the NASA F-18 high alpha research vehicle / Albion H. Bowers [and four others].

    • 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/gpo66569

  • STARS, an integrated, multidisciplinary, finite-element, structural, fluids, aeroelastic, and aeroservoelastic analysis computer program / K.K. Gupta.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, May 1997.
    • 1997-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66581

  • Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements / W. Lance Richards.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, June 1997.
    • 1997-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66583

  • Dynamic ground effect for a cranked arrow wing airplane / Robert E. Curry.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, August 1997.
    • 1997-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66585

  • Supersonic flying qualities experience using the SR-71 / Timothy H. Cox, Dante Jackson.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, August 1997.
    • 1997-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66592

  • Flight demonstration of a shock location sensor using constant voltage hot-film anemometry / Timothy R. Moes, Garimella R. Sarma and Siva M. Mangalam.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, August 1997.
    • 1997-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66599

  • A model for space shuttle orbiter tire side forces based on NASA landing systems research aircraft test results / John F. Carter, Christopher J. Nagy, and Joseph S. Barnicki.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, September 1997.
    • 1997-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66604

  • A conversion of Wheatstone bridge to current-loop signal conditioning for strain gages / Karl F. Anderson.

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, April 1995.
    • 1995-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66608

  • The F/A-18 high-angle-of-attack ground-to-flight correlation, lessons learned / Daniel W. Banks [and six others].

    • 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/gpo65688

  • Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack / Kenneth W. Iliff, Kon-Sheng Charles Wang.

    • Text
    • [Washington, D.C] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program Center, February 1997.
    • 1997-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65693

  • Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing / Sheryll Goecke Powers and Lannie D. Webb.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, June 1997.
    • 1997-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65701

  • Evaluation of high-speed civil transport handling qualities criteria with supersonic flight data / Timothy H. Cox and Dante W. Jackson.

    • 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/gpo65709

  • Overview of recent flight flutter testing research at NASA Dryden / Martin J. Brenner, Richard C. Lind, and David F. Voracek.

    • 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/gpo65710

  • Wavelet analyses of F/A-18 aeroelastic and aeroservoelastic flight test data / Martin J. Brenner.

    • 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/gpo65711

  • A gas chromatograph/mass spectrometer system for ultralow-emission combustor exhaust studies / Chowen Chou Wey and Theodore A. Brabbs.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, June 1996.
    • 1996-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo69218

  • The middeck 0-gravity dynamics experiment / Edward F. Crawley, Marthinus C. Van Schoor, and Edward B. Bokhour ; prepared for Langley Research Center.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, March 1993.
    • 1993-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71475

  • Evaluation of MARC for the analysis of rotating composite blades / Karen F. Bartos and Michael A. Ernst.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, March 1993.
    • 1993-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo77078

  • Lewis Icing Research Tunnel test of the aerodynamic effects of aircraft ground deicing/anti-icing fluids / L. James Runyan [and three others].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, August 1992.
    • 1992-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo76155

  • Extraction of stability and control derivatives from orbiter flight data / Kenneth W. Iliff and Mary F. Shafer.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, June 1993.
    • 1993-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71191

  • NASA publications guide for authors.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, NASA Scientific and Technical Information Program, November 1999.
    • 1999-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo82695

  • NASA publications guide for authors.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, NASA Scientific and Technical Information Program, July 2005.
    • 2005-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo82696

  • ICAN/damp-integrated composite analyzer with damping analysis capabilities : users manual / Dimitrious A. Saravanos, Jose G. Sanfeliz.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, November 1992.
    • 1992-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo150673

  • Simulator evaluation of displays for a revised takeoff performance monitoring system / David B. Middleton, Raghavachari Srivatsan, and Lee H. Person, Jr.

    • Text
    • Washington, DC : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, December 1992.
    • 1992-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo150746

  • Physical properties of the Benchmark Models Program supercritical wing / Bryan E. Dansberry [and five others].

    • Text
    • Washington, DC : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, September 1993.
    • 1993-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo173159

  • Generalized hypercube structures and hyperswitch communication network / Steven D. Young.

    • Text
    • Washington, DC : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, [June 1992]
    • 1992-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo173712

  • Correlation and prediction of dynamic human isolated joint strength from lean body mass / Abhilash K. Pandya [and four others].

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, June 1992.
    • 1992-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo173668

  • Experimental validation of clock synchronization algorithms / Daniel L. Palumbo, R. Lynn Graham.

    • Text
    • Washington, DC : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, [July 1992]
    • 1992-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo173720

  • Effect of temperature and gap opening rate on the resiliency of candidate solid rocket booster O-ring materials / Cynthia L. Lach.

    • Text
    • Washington, DC : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, July 1992.
    • 1992-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo173643

  • Buckling behavior of long symmetrically laminated plates subjected to combined loadings / Michael P. Nemeth.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, May 1992.
    • 1992-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo195860

  • Goddard conference on mass storage systems and technologies : proceedings of a conference held at NASA Goddard Space Flight Center.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.
    • 1992-1992

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