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  • A preliminary design proposal for a maritime patrol strike aircraft [microform] : MPS-200 Condor.

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

  • Flight investigation of the use of a nose gear jump strut to reduce takeoff ground roll distance of STOL aircraft [microform] / Joseph C. Eppel, Gordon Hardy, and James L. Martin.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • V/STOL aircraft configurations and opportunities in the Pacific Basin [microform] / James A. Albers and John Zuk.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Aerodynamics of the Viggen 37 aircraft. Part 1, General -characteristics at low speed [microform] / Krister Karling.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Progress report on Multi-input multi-output system control for experimental aircraft [microform] : NCC2-288, December 13, 1985 / principal investigator, David K. Schmidt.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability [microform] / Mary L. Mason and James R. Burley II.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
    • 1986

  • STOVL propulsion system volume dynamics approximations [microform] / Colin K. Drummond.

    • Text
    • Cleveland, Ohio : Lewis Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS58847

  • Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft [microform] / Barbara S. Esker and Jack G. McArdle ; prepared for the 26th Joint Propulsion Conference cosponsored by the AIAA, ASME, SAE, and ASEE, Orlando, Florida, July 16-18, 1990.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67477

  • 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

  • STOVL aircraft simulation for integrated flight and propulsion controls research [microform] / James R. Mihaloew and Colin K. Drummond ; prepared for the 10th Applied Dynamics International Users Society Annual Conference, Keystone, Colorado, June 25-28, 1989.

    • Text
    • [Cleveland, Ohio?] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69161

  • Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept [microform] / Donald R. Riley and Gautam H. Shah, Richard E Kuhn.

    • 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], 1989.
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS72303

  • In-flight measurements of wing ice shapes and wing section drag increases caused by natural icing conditions [microform] / Kevin Mikkelsen ... [et al.].

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS84279

  • Velocity and temperature decay characteristics of inverted-profile jets [microform] / U. von Glahn, J. Goodykoontz, and C. Wasserbauer.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
    • 1986

  • Development and analysis of a STOL supersonic cruise fighter concept [microform] / Samuel M. Dollyhigh, ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

  • Calculation of vertical and ramp-assisted takeoffs for supersonic cruise fighters [microform] / Grace C. Liu.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

  • National Aerospace Laboratory News (Japan) [microform] / [Jun Takeda].

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1982]
    • 1982

  • Supersonic STOVL aircraft from a propulsion point of view [microform] / R. Luidens, ... [et al.].

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS99449

  • Supersonic STOVL aircraft with turbine bypass/turbo-compressor engines [microform] / Leo C. Franciscus and Roger W. Luidens.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS99531

  • A flight-test evaluation of a go-around control system for a twin-engine powered-lift STOL airplane [microform] / DeLamar M. Watson and Gordon H. Hardy.

    • Text
    • Moffett, Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1983]
    • 1983

  • Propulsion and airframe aerodynamic interactions of supersonic V/STOL configurations, Phase I : final report / M. R. Mraz, P .E. Hiley.

    • Text
    • St. Louis, Mo. : McDonnell Aircraft Company ; Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985]
    • 1985

  • Propulsion and airframe aerodynamic interactions of supersonic V/STOL configurations, Phase I / M.R. Mraz, P.E. Hiley.

    • Text
    • St. Louis, Missouri : McDonnell Aircraft Company ; Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, 1985.
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo34805

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