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  • Navier-Stokes simulation of several high-lift reference H configurations [microform] / Wendy B. Lessard.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]
    • 1999

  • Concept development of a Mach 2.4 high-speed civil transport [microform] / James W. Fenbert ... [et al.].

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

  • Effect of leading- and trailing-edge flaps on clipped delta wings with and without wing camber at supersonic speeds [microform] / Gloria Hernandez ... [et al.].

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

  • Surface documentation of a 3-D supersonic, shock-wave-boundary layer interaction [microform] / Jeffrey K. Wideman ... [et al.].

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

  • Concept development of a Mach 4 high-speed civil transport [microform] / Christopher S. Domack ... [et al].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1990.
    • 1990

  • 1989 high-speed civil transport studies [microform] / HSCT Concept Development Group, Advanced Commercial Programs, Douglas Aircraft Company.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails [microform] / Jerry M. Allen and Carolyn B. Watson.

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

  • High speed civil transport [microform] / Apogee Aeronautics Corporation.

    • Text
    • [Pomona, Calif.] : California State Polytechnic University, Pomona, Aerospace Engineering Dept. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • 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

  • Flow coefficient behavior for boundary layer bleed holes and slots [microform] / B.P. Willis, D.O. Davis, and W. R. Hingst.

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

  • Parametric study on laminar flow for finite wings at supersonic speeds [microform] / Joseph Avila Garcia.

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

  • Experimental investigation of inlet-combustor isolators for a dual-mode scramjet at a Mach number of 4 [microform] / Saied Enami ... [et al.].

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

  • Effect of density gradients in confined supersonic shear layers [microform] / Oshin Peroomian and R.E. Kelly.

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

  • High speed nozzles task [microform] : final report / Awatef Hamed, principal investigator.

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

  • Preliminary airborne measurements for the SR-71 sonic boom propagation experiment [microform] / Edward A. Haering, L.J. Ehernberger, and Stephen A. Whitmore.

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

  • Control effectiveness and tip-fin dihedral effects for the HL-20 lifting-body configuration at Mach numbers from 1.6 to 4.5 [microform] / Christopher I. Cruz and George M. Ware.

    • 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

  • Simulation of crossflow instability on a supersonic highly swept wing [microform] / C. David Pruett.

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

  • 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

  • Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight [microform] / Scott R. Thomas, H. Douglas Perkins, and Charles J. Trefny.

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

  • Computations of axisymmetric flows in hypersonic shock tubes [microform] / Surendra P. Sharma and Gregory J. Wilson.

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

  • Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel [microform] / Richard J. Re and Francis J. Capone.

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

  • Measurements of supersonic wing tip vortices [microform] : 18th AIAA Aerospace Ground Testing Conference, June 20-23, 1994/Colorado Springs, CO / M.K. Smart, I.M. Kalkhoran and J. Bentson.

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

  • Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction [microform] : 32nd Aerospace Sciences Meeting & Exhibit, January 10-13, 1994/Reno, NV / by Jeffrey K. Wideman ... [et al.].

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

  • 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

  • First order ozone impact of a fleet of supersonic business jets (SSBJs) [microform] / Steven L. Baughcum.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2002]
    • 2002

  • Pilot comments for high speed research cycle 3 simulation study (LaRC.1) [microform] / Melvin L. Bailey, editor.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information, [2000]
    • 2000
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS39008

  • Lee-side flow over delta wings at supersonic speeds [microform] / David S. Miller and Richard M. Wood.

    • 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

  • High speed commercial transport fuels considerations and research needs [microform] / C.M. Lee and R.W. Niedzwiecki ; prepared for the Symposium on the Structure of Future Jet Fuels II sponsored by the American Chemical Society, Miami Beach, Florida, September 10-15, 1989.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS62607

  • 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

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  • Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A [microform] / James H. Dittmar.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1985]
    • 1985

  • Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds [microform] / M. Leroy Spearman.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
    • 1986

  • 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

  • Noise of the SR-6 propeller model at 2⁰ and 4⁰ angles of attack [microform] / James H. Dittmar, George L. Stefko, and Robert J. Jeracki.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1983]
    • 1983

  • Supersonic cruise technology [microform] / F. Edward McLean.

    • Text
    • Washington, D.C. : NASA Scientific and Technical Information Branch, National Aeronautics and Space Administration, 1985.
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS101643

  • Analysis of buzz in a supersonic inlet / Rodrick V. Chima.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo30597

  • Design and analysis tool for external-compression supersonic inlets / John W. Slater.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo32321

  • Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds / Harry W. Carlson and Robert J. Mack.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980.
    • 1980-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71124

  • Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight / Scott R. Thomas, H. Douglas Perkins, and Charles J. Trefny.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, March 1997.
    • 1997-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo72111

  • Experimental sonic boom measurements on a Mach 1.6 cruise low-boom configuration / Floyd J. Wilcox, Jr. [and five others].

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo32718

  • In-flight boundary-layer transition on a large flat plate at supersonic speeds / D.W. Banks [and four others].

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37503

  • Highlights from a Mach 4 experimental demonstration of inlet mode transition for Turbine-Based Combined Cycle hypersonic propulsion / Lancert E. Foster [and three others].

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo38254

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