Research Catalog

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  • Experimental and analytical studies of flow through a ventral and axial exhaust nozzle system for STOVL aircraft [microform] / Barbara S. Esker and James R. DeBonis.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • An analysis of cross-coupling of a multi component jet engine test stand using finite element modeling techniques [microform] : final report / by William G. Schweikhard and Werachone N. Singnoi.

    • Text
    • Lawrence, Kan. : University of Kansas ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1995

  • SRM internal flow test and computational fluid dynamic analyses [microform] : final report : contract NAS8-39095 / prepared by ERC, Incorporated.

    • Text
    • Huntsville, AL : ERC, Inc. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995- ]
    • 1995-present

  • Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure [microform] / M. Moin Hussaini and John J. Korte.

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

  • Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure [microform] / Robert S. Jankovsky and John M. Kazaroff, Albert J. Pavli.

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

  • CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system [microform] : final report : under contract NAG3-1500 / Ing Chuang, Louis G. Hunter.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • 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

  • Semi-annual status report on NASA grant NAG 1-837, "Aerodynamics of thrust vectoring" [microform] : June 11, 1989-December 10, 1989 / by J.B. Tseng and C. Edward Lan.

    • Text
    • Lawrence, Kan. : Flight Research Laboratory, University of Kansas Center for Research ; [Washington, D.C. : National Aeronautics and Space Administration, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69319

  • Propulsion and control propellers with thruster nozzles primarily for aircraft applications [microform] / W. Pabst.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1986]
    • 1986

  • An investigation at static conditions of nonaxisymmetric nozzle thrust reverser port geometry including effects of rounding and rotating the port corner [microform] / Dorothy G. Arbiter.

    • Text
    • Hampton, Va. : Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure / M. Moin Hussaini and John J. Korte.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 1996.
    • 1996-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS67205

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