Research Catalog

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  • Application of two procedures for dual-point design of transonic airfoils [microform] / Raymond E. Mineck, Richard L. Campbell, and Dennis O. Allison.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Dynamic ground effects flight test of an F-15 aircraft [microform] / Stephen Corda ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
    • 1994

  • On the use of controls for subsonic transport performance improvement [microform] : overview and future directions / Glenn Gilyard and Martín España.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • 1987 Ground Vortex Workshop [microform] : proceedings of a meeting held at NASA Ames Research Center, Moffett Field, California, April 22-23, 1987 / edited by Richard J. Margason.

    • Text
    • [Moffett Field, CA] : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1988]
    • 1988

  • Development of a low-aspect ratio fin for flight research experiments [microform] / David M. Richwine, John H. Del Frate.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
    • 1994

  • Digital electronic engine control (DEEC) flight evaluation in an F-15 airplane [microform] : proceedings of a minisymposium held at NASA Ames Research Center, Dryden Flight Research Facility, Edwards, California, May 25-26, 1983.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1984.
    • 1984

  • Flight characteristics of the onboard propulsion system model for the performance seeking control algorithm on an F-15 aircraft [microform] / John S. Orme and Gerard S. Schkolnik.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Flight test validation of a frequency-based system identification method on an F-15 aircraft [microform] / Gerard S. Schkolnik, John S. Orme and Mark A. Hreha.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • An electronic workshop on the performance seeking control and propulsion controlled aircraft results of the F-15 Highly Integrated Digital Electronic Control Flight Research Program [microform] : proceedings of the electronic workshop / compiled by Sheryll Geocke Powers.

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

  • F-15B/flight test fixture II [microform] : a test bed for flight research / David M. Richwine.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1997]
    • 1996

  • Key topics for high-lift research [microform] : a joint wind tunnel/flight test approach : report for NASA-Ames University consortium, joint research interchange, May 1, 1995 - September 30, 1996 / collaborators: David Fisher, Flint O. Thomas, and Robert C. Nelson.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Integrated control using the SOFFT control structure [microform] : under contract NAS1-20185 / Nesim Halyo.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Flight demonstration of a shock location sensor using constant voltage hot-film anemometry [microform] / 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 ; [Springfield, Va. : National Technical Information Service, distributor], 1997.
    • 1997

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

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1997.
    • 1997

  • Development and flight evaluation of an emergency digital flight control system using only engine thrust on an F-15 airplane [microform] / Frank W. Burcham, Jr. ... [et. al].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
    • 1996

  • Direct adaptive aircraft control using dynamic cell structure neural networks [microform] / Charles C. Jorgensen.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Full flight envelope direct thrust measurement on a supersonic aircraft [microform] / Timothy R. Conners and Robert L. Sims.

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

  • High stability engine control (HISTEC) flight test results [microform] / Robert D. Southwick ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis 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

  • The high stability engine control (HISTEC) program [microform] : flight demonstration phase / John C. DeLaat ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • The value of early flight evaluation of propulsion concepts using the NASA F-15 research airplane [microform] / Frank W. Burcham, Jr., and Ronald J. Ray.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, VA : National Technical Information Service, distributor], 1987.
    • 1987

  • Application and flight test of linearizing transformations using measurement feedback to the nonlinear control problem [microform] / Robert F. Antoniewicz and Eugene L. Duke, P.K.A. Menon.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67811

  • Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration [microform] / Guy T. Kemmerly.

    • Text
    • [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.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68080

  • A comparison of time-optimal interception trajectories for the F-8 and F-15 [microform] : final report / principal investigator: Anthony J. Calise.

    • Text
    • Atlanta, GA : Georgia Institute of Technology, School of Aerospace Engineering, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69235

  • A preliminary evaluation of an F100 engine parameter estimation process using flight data [microform] / Trindel A. Maine, Glenn B. Gilyard, and Heather H. Lambert.

    • Text
    • 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.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS70364

  • Development of a flight test maneuver autopilot for an F-15 aircraft [microform] / Gurbux S. Alag and Eugene L. Duke.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1985.
    • 1985

  • The development of an airborne instrumentation computer system for flight test [microform] / Glenn A. Bever.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1984.
    • 1984

  • The development of an airborne instrumentation computer system for flight test [microform] / Glenn A. Bever.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1984.
    • 1984

  • Impacts of space shuttle thermal protection system tile on an F-15 aircraft vertical tail [microform] / William L. Ko.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, [1985]
    • 1985

  • Flight evaluation of the DEEC secondary engine control air-start capability [microform] / J. Blair Johnson and Jeff Nelson.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, [1983]
    • 1983

  • Exhaust nozzle plume effects on sonic boom test results for vectored nozzles / Raymond Castner.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo28438

  • Proposed flight research of a dual-bell rocket nozzle using the NASA F-15 airplane / Daniel S. Jones and Trong T. Bui, Joseph H. Ruf.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, September 2013.
    • 2013-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo50963

  • Optimal cooperative control synthesis of active displays / by Sanjay Garg and David K. Schmidt ; submitted to NASA Dryden Flight Research Facility, Ames Research Center.

    • Text
    • Edwards, Calif. : NASA Dryden Flight Research Facility, Ames Research Center, 22 October, 1985.
    • 1985-1022
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo63119

  • Optimal cooperative control synthesis of active displays / by Sanjay Garg and David K. Schmidt ; submitted to NASA Dryden Flight Research Facility, Ames Research Center.

    • Text
    • Edwards, Calif. : NASA Dryden Flight Research Facility, Ames Research Center, 22 October, 1985.
    • 1985-1022

  • 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

  • Flight test results on the stability and control of the F-15 Quiet Spike aircraft / Cheng M. Moua [and three others].

    • Text
    • Edwards, CA : National Aeronautics and, Space Administration, Dryden Flight Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo32721

  • In-flight boundary-layer transition on a large flat plate at supersonic speeds / D.W. Banks [and four others].

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37503

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