Research Catalog

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  • Effect of passive venting on static pressure distributions in cavities at subsonic and transonic speeds [microform] / Robert L. Stallings, Jr. ... [et al.].

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

  • A preliminary look at techniques used to obtain airdata from flight at high angles of attack [microform] / Timothy R. Moes 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, 1990]
    • 1990

  • Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel [microform] / E.B. Plentovich and Blair B. Gloss.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Infomraton Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1986.
    • 1986

  • The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers [microform] / E.B. Plentovich.

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

  • 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

  • Flow through a rectangular-to-semiannular diffusing transition duct [microform] / Jeff Foster ... [et al.].

    • Text
    • [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

  • Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction [microform] / Hyun D. Kim, Warren R. Hingst, and David O. Davis.

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

  • Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows [microform] / J.G. Williams and W.G. Steenken, A.J. Yuhas.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test) [microform] / E. Allen Arrington and Jose C. Gonsalez.

    • 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

  • Rocket-based combined cycle engine technology development [microform] : inlet CFD validation and application / J.R. DeBonis and S. Yungster.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Aeronautics and Space Administration, distributor], 1996.
    • 1996

  • 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

  • PSP measurement of stator vane surface pressures in a high speed fan [microform] / Jan Lepicovsky.

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

  • Design and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment [microform] / Donald Greer ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Study of CFD methods applied to rapidly deforming boundaries [microform] / John W. Slater and Donald Freund and Miklos Sajben.

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

  • Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel [microform] / David M. Schuster.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS22955

  • Digital program for calculating static pressure position error [microform] / J. Blair Johnson, Terry J. Larson, and Jules M. Ficke.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, [1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS104848

  • An airfoil flutter model suspension system to accomdate large static transonic airloads [microform] / Wilmer H. Reed, III.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • An airfoil flutter model suspension system to accommodate large static transonic airloads / Wilmer H. Reed, III.

    • Text
    • Newport News, VA : DEI-Tech, Inc. ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo21276

  • Effect of sweep on cavity flow fields at subsonic and transonic speeds / Maureen B. Tracy ... [and others].

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo30610

  • Flow quality surveys in the settling chamber of the NASA Glenn icing research tunnel (2011 tests) / Laura E. Steen [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2014.
    • 2014-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo57986

  • Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight : comprehensive data report / K. Yamamoto [and four others].

    • Text
    • Cincinnati, Ohio : General Electric Company, Aircraft Engine Business Group, February, 1984.
    • 1984-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo58844

  • Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight : comprehensive data report / K. Yamamoto [and four others].

    • Text
    • Cincinnati, Ohio : General Electric Company, Aircraft Engine Business Group, February, 1984.
    • 1984-2

  • Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction / Hyun D. Kim, Warren R. Hingst, and David O. Davis.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo70927

  • Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles / Jeffery A. Yetter, Laurance D. Leavitt.

    • 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/gpo71384

  • A study of the sonic-boom characteristics of a blunt body at a Mach number of 6 / George C. Ashby, Jr.

    • 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/gpo71442

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

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 1996.
    • 1996-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS68006

  • On hammershock propagation in a supersonic flow field / A. Robert Porro.

    • Text
    • Cleveland Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2002.
    • 2002-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS68703

  • Wind tunnel investigation of passive porosity applied to the leading-edge extension and leading-edge flaps on a slender wing at subsonic speed / Gary E. Erickson.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo81470

  • Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel / David M. Schuster.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2001.
    • 2001-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS22955

  • Experimental investigation of aeroelastic deformation of slender wings at supersonic speeds using a video model deformation measurement technique / Gary E. Erickson.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, [2013]
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo40579

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