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  • A flying qualities study of longitudinal long-term dynamics of hypersonic planes [microform] / Timothy H. Cox ... [et al.].

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

  • A simple analytical aerodynamic model of Langley winged-cone aerospace plane concept [microform] / Bandu N. Pamadi.

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

  • Shock-tunnel combustor testing for hypersonic vehicles [microform] / Mark Loomis.

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

  • Supersonic combustion engine testbed [microform] : heat lightning / D. Hoying ... [et al.]

    • Text
    • Houston, Tex. : Universities Space Research Association ; [Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Trajectory optimization and guidance law development for national aerospace plane applications [microform] : final report, July 1, 1987 to November 30, 1988 / principal investigators, A.J. Calise and G.A. Flandro.

    • Text
    • Atlanta, Ga. : School of Aerospace Engineering, Georgia Institute of Technology ; [Springfield, Va. : National Technical Information Service, distributor 1988]
    • 1988

  • Experimental aerothermodynamic research of hypersonic aircraft [microform] : technical progress report (substitution) for the period October 1, 1988 - March 31, 1989 / prepared by Eloret Institute ... Joseph W. Cleary, principal investigator.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va.? : National Technical Information Service, distributor, 1989]
    • 1989

  • Numerical modeling of a cryogenic fluid within a fuel tank [microform] / Donald S. Greer.

    • 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

  • Advanced hypersonic aircraft design [microform] / Group leader, Rob Utzinger ... [et al.].

    • Text
    • [Columbus, Ohio] : Ohio State University, Aeronautical and Astronautical Engineering ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Static and dynamic friction behavior of candidate high temperature airframe seal materials [microform] / C. DellaCorte ... [et al.].

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

  • Aeropropulsion '87. Session 6, High-speed propulsion technology [microform].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Advanced Hypervelocity Aerophysics Facility Workshop [microform] : proceedings of a workshop sponsored by the National Aeronautics and Space Administration and held at Langley Research Center, Hampton, Virginia, May 10-11, 1988 / compiled by Robert D. Witcofski and William I. Scallion.

    • Text
    • Hampton, Va. : The Center ; [Springfield, Va. : National Technical Information Center, distributor, 1991]
    • 1991

  • Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation [microform] / William L. Ko.

    • 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

  • Materials research for high speed civil transport and generic hypersonics [microform] : metals durability / Paul Schulz and Daniel Hoffman.

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

  • 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

  • Development of advanced methods of trajectory and structural analysis for hypersonic aircraft [microform] : final report, October 1, 1995 - January 31, 1997, NASA Ames Research Center grant NCC2-5165 / Mark D. Ardema, principal investigator.

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

  • Thermostructural behavior of a hypersonic aircraft sandwich panel subjected to heating on one side [microform] / William L. Ko.

    • 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

  • Predictions of thermal buckling strengths of hypersonic aircraft sandwich panels using minimum potential energy and finite element methods [microform] / William L. Ko.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : Available from the National Technical Information Service, 1995]
    • 1995
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60789

  • 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

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  • The application of active controls technology to a generic hypersonic aircraft configuration [microform] / M.G. Gilbert ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69437

  • Selections from "Flug Revue und Flugwelt International" [microform] / Penner, H. ... [et al.].

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

  • Assessment of NASA's aircraft noise prediction capability / Milo D. Dahl, editor.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo31486

  • Aerodynamic characteristics of a hypersonic research airplane concept having a 70̊ swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 / Jim A. Penland, James B. Hallissy, and James L. Dillon.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1979.
    • 1979-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo52191

  • Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation / William L. Ko.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, December 1996.
    • 1996-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65666

  • Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 / Jimmy L. Pittman and Gregory D. Riebe.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
    • 1980-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71373

  • A flying qualities study of longitudinal long-term dynamics of hypersonic planes / Timothy H. Cox [and three others].

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Facility, April 1995.
    • 1995-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo82735

  • 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

  • Fail-safe system for actively cooled supersonic and hypersonic aircraft / Robert A. Jones, Dorothy O. Braswell, and Christine B. Richie.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, January 1975.
    • 1975-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo157933

  • Research in robust control for hypersonic aircraft : progress report #2, 1 December 1992- 31 August 1993 / principal investigator: A.J. Calise.

    • Text
    • [Washington, D.C.] : [National Aeronautics and Space Administration], October 1993.
    • 1993-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo176341

  • Research in robust control for hypersonic aircraft : progress report # 3, 1 September - 28 February 1994 / principal investigator: A.J. Calise.

    • Text
    • [Washington, D.C.] : [National Aeronautics and Space Administration], March 1994.
    • 1994-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo176345

  • Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86 / by Cornelius Driver.

    • Text
    • Washington : National Aeronautics and Space Administration, September 1959.
    • 1959-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo182854

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