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  • Multiphysics simulation of active hypersonic lip cooling [microform] / Matthew E. Melis, Wen-Ping Wang.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • 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

  • Transition at hypersonic speeds [microform] / Mark V. Morkovin.

    • Text
    • Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • SR-SCARLET 1 [microform] : Peregrin / Manoj Tandon ... [et al.].

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

  • Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code [microform] / Kamlesh Kapoor, Bernhard H. Anderson, and Robert J. Shaw.

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

  • Parametric study of shock-induced combustion in a hydrogen air system [microform] / by J.K. Ahuja and S.N. Tiwari (principal investigator).

    • Text
    • Norfolk, Va. : Institute for Computational and Applied Mechanics, Old Dominion University ; Hampton, Va. : NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Spectral solution of the viscous blunt body problem. II, Multidomain approximation [microform] / David A. Kopriva.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • A first scramjet study [microform] / George Emmanuel.

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

  • Mach 10 computational study of a three-dimensional scramjet inlet flow field [microform] / Scott D. Holland.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10 [microform] / Scott D. Holland.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Linthicum Heights, MD : NASA Center for AeroSpace Information, distributor ; Springfield, Va. : National Technical Information Service, distributor, [1995]
    • 1995

  • Performance of an aerodynamic yaw controller mounted on the space shuttle orbiter body flap at Mach 10 [microform] / W.I. Scallion.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Application of CFD to the analysis and design of high-speed inlets [microform] : final report / by William C. Rose.

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

  • A fully implicit time accurate method for hypersonic combustion [microform] : application to shock-induced combustion instability / Shaye Yungster and Krishnan Radhakrishnan.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Supersonic second order analysis and optimization program user's manual [microform] / W.C. Clever.

    • Text
    • Los Angeles, Calif. : Rockwell International Corporation ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1984]
    • 1984

  • Turbulence modeling [microform] / Jorge E. Bardina.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Hypersonic flows as related to the national aerospace plane [microform] / Marvin Kussoy, George P.-G. Huang, F. Menter.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1995]
    • 1995

  • Computational study of flow establishment in hypersonic pulse facilities [microform] / S. Yungster, K. Radhakrishnan.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • 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

  • Computational study of a McDonnell Douglas single-stage-to-orbit vehicle concept for aerodynamic analysis [microform] / Ramadas K. Prabhu.

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

  • Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF [microform] / H. Douglas Perkins, Scott R. Thomas, and William D. Pack.

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

  • Three-dimensional Navier-Stokes simulations with two-equation turbulence models of intersecting shock-waves/turbulent boundary layer at Mach 8.3 [microform] / J.E. Bardina, T.J. Coakley.

    • Text
    • Washington, D.C. : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Physics of interplanetary dust collection with aerogel [microform] : final report and summary of research : NASA grant NAG-9-913, Johnson Space Center, September 30, 1996-March 31, 1998 / William W. Anderson.

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

  • Effect of fin leading edge sweep on shock-shock interaction at Mach 6 [microform] / Scott A. Berry and Robert J. Nowak.

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

  • Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment [microform] / Leslie Gong and W. Lance Richards.

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

  • Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program [microform] / Alexander S. Roudakov and Vyacheslav L. Semenov, John W. Hicks.

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

  • Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements [microform] / W. Lance Richards.

    • 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

  • The NASA Hyper-X Program [microform] / D. Freeman ... [et al.].

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

  • Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept [microform] / David E. Hahne.

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

  • Vulnerability of Space Station Freedom modules [microform] : a study of the effects of module perforation on crew & equipment : final report ... contract NCC8-28, period 09 September 1993-14 March 1995 / by J. Serrano ... [et al.].

    • Text
    • Huntsville, AL : University of Alabama in Huntsville, Aerophysics Research Center ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995- ]
    • 1995-present

  • Real-time method for estimating viscous forebody drag coefficients [microform] / Stephen A. Whitemore ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Hanover, MD : NASA Center for AeroSpace Information [distributor] ; Springfield, Va. : National Technical Information Service [distributor, 2000]
    • 2000

  • Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0 [microform] / Ramadas K. Prabhu ; [prepared ... under contract NAS1-96014].

    • Text
    • Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001

  • Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system [microform] / J.R. DeBonis and C.J. Trefny.

    • 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/LPS23166

  • Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees [microform] / Ramadas K. Prabhu.

    • Text
    • Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS39080

  • Mach 6 flow field surveys beneath the forebody of an airbreathing missile [microform] / Patrick J. Johnston and James L. Hunt.

    • 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

  • Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6 [microform] / Floyd J. Wilcox, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, VA : For sale by the National Technical Information Service, 1995]
    • 1995
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60637

  • On the instability of hypersonic flow past a flat plate [microform] / Nicholas Blackaby, Stephen Cowley, Philip Hall.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60955

  • Mach 10 experimental database of a three-dimensional scramjet inlet flow field [microform] / Scott D. Holland.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, VA : Available from the National Technical Information Service, 1995]
    • 1995
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60779

  • Flow separation in shock wave boundary layer interactions at hypersonic speeds [microform] / A. Hamed.

    • 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/LPS61576

  • 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

  • Nonlinear potential analysis techniques for supersonic/hypersonic aerodynamic design [microform] / V. Shankar and W.C. Clever.

    • Text
    • Los Angeles, Calif. : Rockwell International Corporation ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

  • Comparison of measured and calculated temperatures for a Mach 8 hypersonic wing test structure [microform] / Robert D. Quinn and Roger A. Fields.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, [1986]
    • 1986

  • Iodine Tagging Velocimetry and mechanism in the hypersonic near wake of a MultiPurpose Crew Vehicle / R. Jeffrey Balla.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, July 2013.
    • 2012-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo47609

  • Evaluation of the low-speed stability and control characteristics of a Mach 5.5 Waverider concept / David E. Hahne.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 1997.
    • 1997-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65472

  • Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements / W. Lance Richards.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, June 1997.
    • 1997-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66583

  • Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF / H. Douglas Perkins, Scott R. Thomas, and William D. Pack.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo70728

  • Experimental study of convective heating on the back face and payload of a Hypersonic Inflatable Aerodynamic Decelerator (HIAD) aeroshell / Brian R. Hollis [and three others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2017.
    • 2017-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo79528

  • The NASA Hyper-X Program / D. Freeman [and four others].

    • Text
    • [Hampton, VA] : [National Aeronautics and Space Administration, Langley Research Center], [1997]
    • 1997
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo82621

  • Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system / J.R. DeBonis and C.J. Trefny.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2001.
    • 2001-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS23166

  • Quantitative global heat transfer in a Mach-6 quiet tunnel / John P. Sullivan [and ten others].

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo32903

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