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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

  • Two-dimensional converging-diverging rippled nozzles at transonic speeds [microform] / John R. Carlson and Scott C. Asbury.

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

  • Measurements of unsteady pressure and structural response for an elastic supercritical wing [microform] / Clinton V. Eckstrom, David A. Seidel, and Maynard C. Sandford.

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

  • In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft) [microform] / Edwin J. Saltzman, John W. Hicks.

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

  • Transonic aeroelastic analysis of launch vehicle configurations [microform] / João Luiz Filgueiras de Azevedo.

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

  • 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

  • A fully implicit time accurate method for hypersonic combustion [microform] : application to shock-induced combustion instability / Shaye Yungster and Krishnan Radhakrishnan.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane [microform] / Dennis O. Allision and William G. Sewall.

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

  • Validation of the NPARC code for nozzle afterbody flows at transonic speeds [microform] / James R. DeBonis and Nicholas J. Georgiadis, Crawford F. Smith.

    • Text
    • [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

  • PARC3D calculations of the F/A-18A HARV inlet vortex generators [microform] / Steve D. Podleski.

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

  • Flight demonstration of a shock location sensor using constant voltage hot-film anemometry [microform] / Timothy R. Moes, Garimella R. Sarma and Siva M. Mangalam.

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

  • Response of high subsonic jet to nonaxisymmetric disturbances [microform] / A. Bayliss, L. Maestrello.

    • 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

  • Comparison of the aerodynamic characteristics of similar models in two size wind tunnels at transonic speeds [microform] / Anthony M. Springer.

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

  • Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method [microform] : EUROMECH-Colloquium 349, simulation of fluid-structure interaction in aeronautics, Göttingen, Germany, September 16-18, 1996 / John W. Edwards.

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

  • Cavity unsteady-pressure measurements at subsonic and transonic speeds [microform] / Maureen B. Tracy and E.B. Plentovich.

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

  • Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds [microform] / John E. Lamar ... [et al.].

    • 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/LPS26671

  • Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration [microform] / Lawrence E. Putnam.

    • 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

  • Flow unsteadiness effects on boundary layers [microform] / by Sreedhara V. Murthy.

    • Text
    • [Moffett Field, Calif. : NASA Ames Research Center, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60942

  • Final report on investigation of transonic flow over segmented slotted wind tunnel wall with mass transfer [microform] / by M.K. Bhat, A.D. Vakili, and J.M. Wu.

    • Text
    • Tullahoma, TN : The University of Tennessee Space Institute ; [Moffett Field, CA] : NASA Ames Research Center ; [Springfield, VA :: For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS64316

  • An experimental investigation of propfan installations on an unsewpt supercritical wing at transonic Mach numbers [microform] / Glynn R. Bartlett.

    • Text
    • Hampton, Va. : Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS88314

  • Transonic calculation of airfoil stability and response with active controls [microform] / J. T. Batina, T. Y. Yang.

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

  • Numerical simulation of the tip vortex off a low-aspect-ratio wing at transonic speed [microform] / N.N. Mansour.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1984]
    • 1984

  • An experimental documentation of trailing-edge flows at high Reynolds number [microform] / P. R. Viswanath, J. W. Cleary, and H. L. Seegmiller.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1983]
    • 1983

  • Geometric and structural properties of a rectangular supercritical wing oscillated in pitch for measurement of unsteady transonic pressure distributions [microform] / Rodney H. Ricketts ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983]
    • 1983

  • A tomographic technique for aerodynamics at transonic speeds [microform] / George Lee.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985]
    • 1985

  • Flight demonstration of a shock location sensor using constant voltage hot-film anemometry / Timothy R. Moes, Garimella R. Sarma and Siva M. Mangalam.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, August 1997.
    • 1997-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo66599

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

    • Text
    • [Washington, DC] : [National Aeronautics and Space Administration], [1996]
    • 1996
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo78886

  • Wind tunnel investigation of passive vortex control and vortex-tail interactions on a slender wing at subsonic and transonic speeds / 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/gpo40586

  • Effect of canard position and wing leading-edge flap deflection on wing buffet at transonic speeds / by Blair B. Gloss, William P. Henderson, and Jarrett K. Huffman.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, April 1975.
    • 1975-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo157696

  • Stability and control characteristics at transonic speeds of a model of a supersonic target drone with differentially deflected horizontal-tail surfaces / by Dewey E. Wornom.

    • Text
    • Washingon : National Aeronautics and Space Administration, March 1961.
    • 1961-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo173089

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