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  • Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8 [microform] / Mark C. Davis ... [et al.].

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

  • Supersonic symposium [microform] : the men of Mach 1 / edited and with an introduction by James O. Young.

    • Text
    • [Edwards Air Force Base, Calif.] : Air Force Flight Test Center History Office, [1990]
    • 1990

  • Effect of pressure gradient on first mode of instability in high-speed boundary layers [microform] / Jamal A. Masad, Yousef H. Zurigat.

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

  • 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

  • An implementation of a chemical and thermal nonequilibrium flow solver on unstructured meshes and application to blunt bodies [microform] / Ramadas K. Prabhu.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1994]
    • 1994

  • 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

  • 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

  • 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

  • A shadowgraphic study of the national launch system's 1 1/2 stage vehicle configuration and heavy lift launch vehicle configuration [microform] / Darlene C. Pokora and Anthony M. Springer.

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

  • The effects of viscosity on the stability of a trailing-line vortex in compressible flow [microform] / Jillian A.K. Stott, Peter W. Duck.

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

  • Research in robust control for hypersonic vehicles [microform] : progress report #1 / principal investigator: A.J. Calise.

    • Text
    • Atlanta, Ga. : School of Aerospace Engineering, Georgia Institute of Technology ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas [microform] / Robert J. Mack, Kathy E. Needleman.

    • 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

  • A preliminary design study of supersonic through-flow fan inlets [microform] / Paul J. Barnhart.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Performance of the 0.3-meter transonic cryogenic tunnel with air, nitrogen, and sulfer hexafluoride media under closed loop automatic control [microform] / S. Balakrishna and W. Allen Kilgore.

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

  • Comparison of computational and experimental results for a supercritical airfoil [microform] / Melissa B. Rivers and Richard A. Wahls.

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

  • Wing pressure distributions from subsonic tests of a high-wing transport model [microform] / Zachary T. Applin and Carl L. Gentry, Jr., M.A. Takallu.

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

  • 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

  • Measurement of gust response on a turbine cascade [microform] : / A.P. Kurkov and B.L. Lucci.

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

  • Experimental study of a generic high speed civil transport [microform] : tabulated data / Pamela S. Belton and Richard L. Campbell.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Measurements of store forces and moments and cavity pressures for a generic store in and near a box cavity at subsonic and transonic speeds [microform] / Robert L. Stallings ... [et al.].

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

  • On the modulational instability of large amplitude waves in supersonic boundary layers [microform] / Philip Hall, Demetrious T. Papageorgiou.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20 [microform] / Lawrence E. Putnam and Charles E. Mercer.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1986.
    • 1986

  • Molecular dynamics simulation of a piston driven shock wave in a hard sphere gas [microform] / Myeung-Jouh Woo and Isaac Greber.

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

  • Fundamental study of flow field generated by rotorcraft blades [microform] / S.P. Parthasarathy, Y.I. Cho, L.H. Back.

    • Text
    • Pasadena, Calif. : National Aeronautics and Space Administration, Jet Propulsion Laboratory, California Institute of Technology ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Thermal analysis and design of a cooling system for a Mach 14 nozzle [microform] : final report covering period February, 1986 to January, 1987 / prepared by Ronald Mullisen, principal investigator ; Keith Kaste.

    • Text
    • Moffett Field, CA : Thermodynamics Facilities Branch, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • High-resolution shock capturing scheme for high Mach number internal flow [microform] / Seokkwan Yoon and Antony Jameson.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Control of unsteady separated flow associated with the dynamic stall of airfoils [microform] : final report, 95-09 / M.C. Wilder.

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

  • Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept [microform] / A.M. Springer.

    • Text
    • MSFC, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center ; [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

  • User manual for NASA Lewis 10- by 10-foot supersonic wind tunnel [microform] / Ronald H. Soeder.

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

  • Evaluation of F/A-18A HARV inlet flow analysis with flight data [microform] / C. Frederic Smith ... [et al.].

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

  • A longitudinal aerodynamic data repeatability study for a commercial transport model test in the National Transonic Facility [microform] / R.A. Wahls ... [et al.].

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

  • An interactive software for conceptual wing flutter analysis and parametric study [microform] / Vivek Mukhopadhyay.

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

  • Euler/Navier-Stokes flow computations on flexible configurations for stability analysis [microform] / G. Guruswamy and E. Tu.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, American Institute of Aeronautics and Astronautics ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1995

  • 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

  • On the coupling between a supersonic boundary layer and a flexible surface [microform] : final report / Abdelkader Frendi.

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

  • Aerodynamic characteristics of two waverider-derived hypersonic cruise configurations [microform] / Charles E. Cockrell, Jr. and Lawrence D. Huebner, Dennis B. Finley.

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

  • Screech tones of supersonic jets from bevelled rectangular nozzles [microform] / Christopher K.W. Tam and Hao Shen, Ganesh Raman.

    • Text
    • Reston, VA : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 [microform] / Richard J. Re and William K. Abeyounis.

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

  • Wind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing [microform] / Brenda E. Gile Laflin ... [et al.].

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

  • Experimental investigation of plume-induced flow separation on the National Launch System 1¹/₂-stage launch vehicle [microform] : 32nd Aerospace Sciences meeting & exhibit, January 10-13, 1994, Reno, NV / A. Springer.

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

  • A correlation between flight-determined derivatives and wind-tunnel data for the X-24B research aircraft [microform] / Alex G. Sim.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Interaction of a shock with a longitudinal vortex [microform] / Gordon Erlbacher, M.Y. Hussaini, Chi-Wang Shu.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Consistent initial conditions for the DNS of compressible turbulence [microform] / J.R. Ristorcelli, G.A. Blaisdell.

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

  • Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method [microform] / John W. Edwards.

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

  • Near-optimal operation of dual-fuel launch vehicles [microform] / M. Ardema and H.-C. Chou, J. Bowles.

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

  • Computational aeroservoelastic analysis with an Euler-based unsteady flow solver [microform] : NASA-Ames university consortium cooperative agreement no. NCC2-5105, final research summary for the period: 1 November 1994 - 31 January 1997 / principal investigator, Andrew S. Arena, Jr.

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

  • Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D [microform] / S. Paul Pao, Khaled S. Abdol-Hamid.

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

  • Investigation of mixing a supersonic stream with the flow downstream of a wedge [microform] : NCC2-5190 final report / Joseph Sheeley.

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

  • Experimental investigation of unsteady shock wave turbulent boundary layer interactions about a blunt fin [microform] / by Paul J. Barnhart and Isaac Greber.

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

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