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  • Turbulence model comparisons for a high-speed aircraft [microform] / Melissa B. Rivers and Richard A. Wahls.

    • 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

  • Flight test measurements from the Tu-144LL structure/cabin noise experiment [microform] / Stephen A. Rizzi, Robert G. Rackl, Eduard V. Andrianov.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 2000]
    • 2000

  • Development of techniques for the in situ observation of OH and HO₂ for studies of the impact of high-altitude supersonic aircraft on the stratosphere [microform] : final technical report / James G. Anderson, principal investigator.

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

  • STOVL Control Integration Program [microform] / C. Weiss, P. McDowell and S. Watts.

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

  • RTJ-303 [microform] : variable geometry, oblique wing supersonic aircraft / Albert Antaran ... [et al.].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • 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

  • 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

  • Effect of emerging technology on a convertible, business/interceptor, supersonic-cruise jet / F.L. Beissner ... [et al.].

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

  • Supersonic wing and wing-body shape optimization using an adjoint formulation [microform] / James Reuther and Antony Jameson.

    • Text
    • [Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Planar imaging of hydroxyl in a high temperature, high pressure combustion facility [microform] / Yolanda R. Hicks ... [et al.].

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

  • Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on parallel computers [microform] / James Reuther ... [et al.].

    • Text
    • [Moffett Field, CA] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Parallelization of a parabolized Navier-Stokes solver with a design optimizer [microform] : 34th AIAA Aerospace Sciences Meeting and Exhibit / J.M. Pallis and J.J. Chattot, S.L. Lawrence.

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

  • Lateral-directional eigenvector flying qualities guidelines for high performance aircraft [microform] / John B. Davidson, Dominick Andrisani, II.

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

  • Changing the landscape of civil aviation [microform] / Carol J. Russo.

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

  • 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

  • Full flight envelope direct thrust measurement on a supersonic aircraft [microform] / Timothy R. Conners and Robert L. Sims.

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

  • Advances in experiment design for high performance aircraft [microform] : paper no. 8 / Engene A. Morelli.

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

  • Aerodynamic parameters of high performance aircraft estimated from wind tunnel and flight test data [microform] / Vladislav Klein and Patrick C. Murphy.

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

  • Evaluation of frameworks for HSCT design optimization [microform] / Ramki Krishnan.

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

  • Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models [microform] / Eric F. Charlton.

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

  • Progress toward national aeronautics goals [microform] / Carlo J. Russo and Arun K. Sehra.

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

  • Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 [microform] / Francis J. Capone and E. Ann Bare, Dorothy Arbiter.

    • 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

  • Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets [microform] / Charles J. Trefny and Joseph W. Wasserbauer.

    • 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

  • Interactive calculation procedures for mixed compression inlets [microform] / Eli Reshotko.

    • Text
    • Cleveland, Ohio : Dept. of Mechanical and Aerospace Engineering, School of Engineering, Case Institute of Technology, Case Western Reserve University, [1983]
    • 1983
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60916

  • Calculation of vertical and ramp-assisted takeoffs for supersonic cruise fighters [microform] / Grace C. Liu.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

  • Supersonic STOVL aircraft from a propulsion point of view [microform] / R. Luidens, ... [et al.].

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS99449

  • Feasibility and benefits of laminar flow control on supersonic cruise airplanes [electronic resource] / A.G. Powell, S. Agrawal, T. R. Lacey.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS113610

  • Feasibility and benefits of laminar flow control on supersonic cruise airplanes [microform] / A.G. Powell, S. Agrawal, T. R. Lacey.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS113610

  • Exploratory low-speed wind-tunnel study of concepts designed to improve aircraft stability and control at high angles of attack [microform] / by David Edgar Hahne.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1985]
    • 1985

  • PIV measurements of supersonic internally-mixed dual-stream jets / James E. Bridges and Mark P. Wernet.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo26296

  • Exhaust nozzle plume effects on sonic boom test results for isolated nozzles / Raymond S. Castner ; prepared for the 28th Applied Aerodynamics Conference sponsored by the American Institute of Aeronautics and Astronautics, Chicago, Illinois, June 28-July 1, 20.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo27499

  • Exhaust nozzle plume effects on sonic boom test results for vectored nozzles / Raymond Castner.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo28438

  • 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

  • The impact of subsonic twin jets on airport noise / Richard F. Bozark.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo32088

  • Propulsion and airframe aerodynamic interactions of supersonic V/STOL configurations, Phase I : final report / M. R. Mraz, P .E. Hiley.

    • Text
    • St. Louis, Mo. : McDonnell Aircraft Company ; Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985]
    • 1985

  • Propulsion and airframe aerodynamic interactions of supersonic V/STOL configurations, Phase I / M.R. Mraz, P.E. Hiley.

    • Text
    • St. Louis, Missouri : McDonnell Aircraft Company ; Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, 1985.
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo34805

  • Enabling rapid and robust structural analysis during conceptual design / Lloyd B. Eldred, Sharon L. Padula, and Wu Li.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, February 2015.
    • 2015-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo57878

  • Experimental and computational sonic boom assessment of Lockheed-Martin N+2 low boom models / Susan E. Cliff [and four others].

    • Text
    • Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, January 2015.
    • 2015-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo60802

  • Propulsion system dynamic modeling of the NASA supersonic concept vehicle for aeropropulsoservoelasticity / George Kopasakis, Joseph W. Connolly, and Jonathan Seidel.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2016.
    • 2016-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66962

  • 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

  • Vertical tail buffeting alleviation using piezoelectric actuators : some results of the Actively Controlled Response of Buffet-Affected Tails (ACROBAT) program / Robert W. Moses.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, April 1997.
    • 1997-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS60727

  • Numerical simulations of a Quiet SuperSonic Technology (QueSST) aircraft preliminary design / David J. Friedlander, Christopher M. Heath, and Raymond S. Castner.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2018.
    • 2018-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo111274

  • Global environmental impact of supersonic cruise aircraft in the stratosphere / Raymond L. Speth [and seven others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2021.
    • 2021-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo151988

  • Jet noise reduction potential from emerging variable cycle technologies / Brenda S. Henderson, James E. Bridges, and Mark P. Wernet.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo39372

  • Performance and environmental assessment of an advanced aircraft with open rotor propulsion / Mark D. Guynn [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/gpo40597

  • 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

  • Supersonic aerodynamic characteristics of a circular body Earth-to-orbit vehicle / George M. Ware and Walter C. Engelund, Ian O. MacConochie.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January 1994.
    • 1994-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo157682

  • THE PROBLEMS OF DESIGNING FOR THE TAKE-OFF AND LANDING OF HIGH-SPEED AIRCRAFT,

    • Text
    • Ft. Belvoir Defense Technical Information Center JAN 1963.
    • 1963
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-413Off-site

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