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  • High Reynolds number research : a workshop / sponsored by Joint Institute for Advancement of Flight Sciences, the George Washington University, and NASA Langley Research Center and held at Hampton, Virginia, October 27-28, 1976 ; edited by Donald D. Baals.

    • Text
    • Washington : Scientific and Technical Information Office, National Aeronautics and Space Administration ; Springfield, Va. : for sale by National Technical Information Service, 1977.
    • 1977
    • 1 Item
    FormatCall NumberItem Location
    Text JSF 78-218Offsite

  • Transonic dynamics tunnel force and pressure data acquired on the HSR rigid semispan model [microform] / David M. Schuster and Russ D. Rausch.

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

  • 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

  • Tables for correcting airfoil data obtained in the Langley 0.3-meter transonic cryogenic tunnel for sidewall boundary layer effects [microform] / Renaldo V. Jenkins, Jerry B. Adcock.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
    • 1986-1986

  • Investigation of the aeroelastic stability of the AFW wind-tunnel model using CAP-TSD [microform] / Walter A. Silva and Robert M. Bennett.

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

  • Mass flux similarity for slotted transonic-wind-tunnel walls [microform] / Joel L. Everhart, Suresh H. Goradia.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1991.
    • 1991

  • User guide for WAICX [microform] : a transonic wind-tunnel wall interference assessment and correction procedure for the NTF / Javier A. Garriz, Kara J. Haigler.

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

  • High Reynolds number test of the Boeing TR77 airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel [microform] / Julio Chu ... [et al.].

    • Text
    • [Washington, DC] : 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

  • Transonic wind tunnel test of a 14% thick oblique wing [microform] / Robert A. Kennelly, Jr. ... [et al.].

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990

  • Data reduction formulas for the 16-foot transonic tunnel NASA Langley Research Center [microform] / Charles E. Mercer ... [et al.].

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

  • Further buffeting tests in a cryogenic wind tunnel [microform] / D.G. Mabey, R.P. Boyden, and W.G. Johnson, Jr.

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

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

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992.
    • 1992

  • Calibration of the 13- by 13-inch adaptive wall test section for the Langley 0.3-Meter Transonic Cryogenic Tunnel [microform] / Raymond E. Mineck and Acquilla S. Hill.

    • Text
    • [Washington, DC] : 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

  • Electrical noise reduction techniques contributing to improved data quality at the National Transonic Facility [microform] / J.R. McPhee.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1988.
    • 1988

  • Sidewall boundary-layer measurements with upstream suction in the Langley 0.3-meter transonic cryogenic tunnel [microform] / A.V. Murthy.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1988.
    • 1988

  • Slotted-wall flow-field measurements in a transonic wind tunnel [microform] / Joel L. Everhart, William B. Igoe, and Stuart G. Flechner.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1991.
    • 1991

  • Characteristics of vertical and lateral tunnel turbulence measured in air in the Langley Transonic Dynamics Tunnel [microform] / Robert K. Sleeper ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Further investigations of the aeroelastic behavior of the AFW wind-tunnel model using transonic small disturbance theory [microform] / Walter A. Silva and Robert M. Bennett.

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

  • Experimental study of a generic high speed civil transport-tabulated data [microform] / 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

  • The NASA Langley Research Center 0.3-meter Transonic Cryogenic Tunnel microcomputer Controller source code [microform] / W. Allen Kilgore and S. Balakrishna.

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

  • A feasibility study of using Langley 0.3-m Transonic Cryogenic Tunnel sidewall boundary-layer removable system for heavy gas testing [microform] / A.V. Murthy, S. Balakrishna, and W. Allen Kilgore.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • NASA Lewis 8- by 6-foot supersonic wind tunnel user manual [microform] / Ronald H. Soeder.

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

  • Wall interference and boundary simulation in a transonic wind with a discretely slotted test section [microform] / Jassim A. Al-Saadi.

    • 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

  • Analysis of fluctuating static pressure measurements in a large high Reynolds number transonic cryogenic wind tunnel [microform] / by William B. Igoe.

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

  • A study of residual interference effects in adaptive wall testing of a 7-inch chord CAST-10-2/DOA 2 airfoil model [microform] / A.V. Murthy.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991

  • High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions [microform] / Julio Chu and Pierce L. Lawing.

    • Text
    • [Washington, DC] : 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

  • High Reynolds number tests of a NASA SC(3)-0712(b) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnels [microform] / William G. Johnson, Jr., Acquilla S. Hill, and Otto Eichmann.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1985.
    • 1985

  • Flow quality of NAL two-dimensional transonic wind tunnel. Part I, Mach number distributions, flow angularities, and preliminary study of side wall boundary layer suction [microform] / Seizo Sakakibara ... [et al.].

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

  • Results for the hybrid laminar flow control experiment conducted in the NASA Langley 3-FT transonic pressure tunnel on a 7-ft chord model [microform] / Percy J. Bobbitt ... [et al.].

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

  • Description and evaluation of an interference assessment method for a slotted-wall wind tunnel [microform] / William B. Kemp, Jr.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1991.
    • 1991

  • Experimental uncertainty and drag measurements in the National Transonic facility [microform] / Stephen M. Batill.

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

  • The NASA Langley 8-foot transonic pressure tunnel calibration [microform] / Cuyler W. Brooks, Charles D. Harris, and Patricia G. Reagon.

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

  • Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability [microform] / George T. Carson, Jr., and Francis J. Capone.

    • 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], 1991.
    • 1991

  • A user's guide to the Langley 16-foot transonic tunnel complex [microform] / Staff of the Aerodynamics Branch.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Two experimental supercritical laminar-flow-control swept-wing airfoils [microform] / Dennis O. Allison and J. Ray Dagenhart.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Performance of the active sidewall boundary-layer removal system for the Langley 0.3-meter transonic cryogenic tunnel [microform] / S. Balakrishna, W. Allen Kilgore, and A.V. Murthy.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Microcomputer based controller for the Langley 0.3-meter Transonic Cryogenic Tunnel [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, 1989]
    • 1989

  • Experimental/analytical approach to understanding mistuning in a transonic wind tunnel compressor [microform] / Teri Kaiser ... [et al.].

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

  • 16-foot transonic tunnel test section flowfield survey [microform] / J.A. Yetter and W.K. Abeyounis.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1994

  • 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

  • A simplified fourwall interference assessment procedure for airfoil data obtained in the Langley 0.3-meter transonic cryogenic tunnel [microform] / A.V. Murthy.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1987.
    • 1987

  • Correlation of transonic-cone Preston-tube data and skin friction [microform] : final report (research grant number NAG 2-76) (Nov. 80 - May 84) / prepared by A. S. Abu-Mostafa and T.D. Reed.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1984]
    • 1984

  • Experimental analyses of trailing edge flows [microform] : final technical report to NASA Ames Research Center / S.L. Petrie, D.S. Emmer.

    • Text
    • [Moffett Field, Calif.] : The Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986?]
    • 1986

  • Development of a model protection and dynamic response monitoring system for the National Transonic Facility [microform] / Clarence P. Young, Jr., S. Balakrishna, W. Allen Kilgore.

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

  • Transonic interference reduction by limited ventilation wall panels [microform] / John D. Lee.

    • Text
    • Cleveland, Ohio : Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Derivation of jack movement influence coefficients as a basis for selecting wall contours giving reduced levels of interference in flexible walled test sections [microform] / M.J. Goodyer.

    • Text
    • Hampton, VA : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1985]
    • 1985

  • The status of two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel [microform] / Mark C. Lewis.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1985.
    • 1985

  • Computer model to simulate testing at the National Transonic Facility [microform] / Raymond E. Mineck ... [et al.].

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

  • A concept for transition mapping on a 10⁰-cone in the National Transonic Facility using flow-pressure variation [microform] / Ehud Gartenberg.

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

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