Research Catalog

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  • A low-erosion starting technique for high-performance arcjets [microform] / John M. Sankovic and Francis M. Curran.

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

  • Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream [microform] / George C. Olsen and Robert J. Nowak.

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

  • RSRM 10% Scale Model drilled hole plate tests [microform] : final report, contract NAS8-40347 / prepared by ERC, Incorporated, Huntsville Operation.

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

  • User's manual for FOMOCO utilities-force and moment computation tools for overset grids [microform] / William M. Chan, Pieter G. Buning.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction [microform] / Hyun D. Kim, Warren R. Hingst, and David O. Davis.

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

  • [Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests] [microform] / [Holzman, Jon K.].

    • Text
    • [Edwards, Calif. : NASA Dryden Flight Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • High voltage SPT performance [microform] / David Manzella, David Jacobson and Robert Jankovsky.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS30009

  • Calibration of sonic valves for the laminar flow control, leading-edge flight test [microform] / Dennis H. Petley ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service,] 1985.
    • 1985

  • Ultra-efficient engine diameter study [microform] / David L. Daggett, Stephen T. Brown, and Ron T. Kawai.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55129

  • Computational analyses of the LIMX TBCC inlet high-speed flowpath / Vance F. Dippold, III.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo25003

  • Thermosyphon flooding in reduced gravity environments / Marc Andrew Gibson.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2013.
    • 2013-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53614

  • Generalized Fluid System Simulation Program, version 6.0 / A.K. Majundar [and three others].

    • Text
    • Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, October 2013.
    • 2013-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53733

  • Computational aerodynamic simulations of a 1484 ft/sec tip speed quiet high-speed fan system model for acoustic methods assessment and development / Daniel L. Tweedt.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2014.
    • 2014-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo55842

  • Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction / Hyun D. Kim, Warren R. Hingst, and David O. Davis.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, December 1996.
    • 1996-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70927

  • Multiple-cycle simulation of a pulse detonation engine ejector / S. Yungster, H.D. Perkins.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2002.
    • 2002-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS53266

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