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  • Experimental investigation of nozzle/plume aerodynamics at hypersonic speeds [microform] / David W. Bogdanoff.

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

  • Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0 [microform] / Ira J. Walker, Peter F. Covell And Dana K. Forrest.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
    • 1993

  • Hypersonic turbulent boundary-layer and free shear database [microform] / Gary S. Settles and Lori J. Dodson.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1994

  • Thermal and structural assessments of a ceramic wafer seal in hypersonic engines [microform] / Mike T. Tong and Bruce M. Steinetz.

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

  • An approximate Riemann solver for thermal and chemical nonequilibrium flows [microform] / Ramadas K. Prabhu.

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

  • Evaluation and ranking of candidate ceramic wafer engine seal materials [microform] / Bruce M. Steinetz.

    • Text
    • [Washington, DC] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991

  • A dynamic response model for pressure sensors in continuum and high Knudsen number flows with large temperature gradients [microform] / Stephen A. Whitmore, Brian J. Petersen, David D. Scott.

    • 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

  • Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration [microform] / W.P. Phillips and W.C. Engelund.

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

  • Magnetohydrodynamics Accelerator Research into Advanced Hypersonics (MARIAH) [microform] : final report / Jack A. Baughman ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service [distributor, 1997]
    • 1997

  • Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel [microform] / Glen P. Doggett and Ndaona Chokani.

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

  • Systems challenges for hypersonic vehicles [microform] : [AGARD] paper C37 / by James L. Hunt and Gerard Laruelle and Alain Wagner.

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

  • Airbreathing hypersonic systems focus at NASA Langley Research Center [microform] / James L. Hunt and Vincent L. Rausch.

    • Text
    • Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies [microform] / Irina G. Brykina, Carl D. Scott.

    • Text
    • Houston, Tex. : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Hypersonic boundary-layer transition for X-33 phase II vehicle [microform] / R.A. Thompson ... [et al.].

    • Text
    • Reston, Va. : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • The kinetic nonequilibrium processes in the internal flow and in the plume of subsonic and supersonic aircrafts [microform] : summary of research, from August 28, 1996 to August 28, 1997, NAG3-1957 / Alexander M. Starik.

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

  • The X-33 extended flight test range [microform] / Dale A. Mackall, Robert Sakahara, Steven E. Kremer.

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

  • Aeroheating predictions for X-34 using an inviscid-boundary layer method [microform] / Christropher J. Riley and William L. Kleb.

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

  • Development of the X-33 aerodynamic uncertainty model [microform] / Brent R. Cobleigh.

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

  • Multidisciplinary analysis of a hypersonic engine [microform] / M.E.M. Stewart ... [et al.] ; prepared for the 11th International Conference on Space Planes and Hypersonic Systems and Technologies ... September 29-October 4, 2002.

    • 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, 2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS42592

  • Structures and materials technology for hypersonic aerospacecraft [microform] / Harvey G. McComb, Jr., Harold N. Murrow, and Michael F. Card.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67910

  • Prediction of forces and moments for flight vehicle control effectors [microform] / M. Maughmer ... [et al.].

    • Text
    • Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 2 Resources

    Available Online

    See All Available Online Resources

  • Optimal trajectories for an aerospace plane [microform] / by A. Miele, W.Y. Lee, and G.D. Wu.

    • Text
    • Houston, Tex. : Rice University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990
    • 2 Resources

    Available Online

    See All Available Online Resources

  • Current capabilities and future directions in computational fluid dynamics [electronic resource] / Committee to Assess Current Capabilities and Future Directions in Computational Fluid Dynamics, Aeronautics and Space Engineering Board, Commission on Engineering and Technical Systems, National Research Council.

    • Text
    • Washington, D.C. : National Academy Press : Available from Aeronautics and Space Engineering Board, National Research Council, 1986.
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS113728

  • Current capabilities and future directions in computational fluid dynamics [microform] / Committee to Assess Current Capabilities and Future Directions in Computational Fluid Dynamics, Aeronautics and Space Engineering Board, Commission on Engineering and Technical Systems, National Research Council.

    • Text
    • Washington, D.C. : National Academy Press : Available from Aeronautics and Space Engineering Board, National Research Council, 1986.
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS113728

  • Preliminary structural sensitivity study of hypersonic inflatable aerodynamic decelerator using probabilistic methods / Karen H. Lyle.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, July 2014.
    • 2014-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo55362

  • Comparison of analysis with test for static loading of two hypersonic inflatable aerodynamic decelerator concepts / Karen H. Lyle.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, July 2015.
    • 2015-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo62835

  • Multidisciplinary analysis of a hypersonic engine / M.E.M. Stewart [and four others].

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

    Available Online

    https://purl.fdlp.gov/GPO/LPS42592

  • An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies / Irina G. Brykina, Carl D. Scott.

    • Text
    • Houston, Texas : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, May 1998.
    • 1998-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo83038

  • Solution-space screening of a hypersonic endurance demonstrator / Bernd Chudoba [and four others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37147

  • Operational experience in the Langley Expansion Tube with various testy gases / Charles G. Miller.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 1977.
    • 1977-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo173927

  • Hypersonic aerodynamic characteristics of a model of low-fineness-ratio variable-geometry logistics spacecraft concept / by Bernard Spencer.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, December 1968.
    • 1968-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo182851

  • Transonic aerodynamic characteristics of two hypersonic cruise configurations / by Richard A. Langhans.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, June 1969.
    • 1969-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo182861

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