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  • 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

  • Asymptotic behavior of a flat plate wake [microform] / by James H. Weygandt and Rabindra D. Mehta.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Development of direct-inverse 3-D method for applied aerodynamic design and analysis [microform] : semiannual progress report, July 1, 1986 - December 31, 1986 / Leland A. Carlson.

    • Text
    • College Station, Tex. : Texas Engineering Experiment Station, Aerospace Engineering Department, Texas A&M University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Viscous wing theory development [microform] : final report.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • 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

  • An improved viscid/inviscid interaction procedure for transonic flow over airfoils [microform] / R.E. Melnik ... [et al.].

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

  • 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

  • An experimental study of a turbulent boundary layer in the trailing edge region of a circulation-control airfoil [microform] / Jeff Brown.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1995]
    • 1995

  • High-lift systems on commercial subsonic airliners [microform] / Peter K.C. Rudolph.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Assessment of dual-point drag reduction for an executive-jet modified airfoil section [microform] / Dennis O. Allison and Raymond E. Mineck.

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

  • Optimum transonic airfoils based on the Euler equations [microform] / Angelo Iollo, Manuel D. Salas.

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

  • An experimental investigation of the confluent boundary layer on a high-lift system [microform] : final project report / by F.O. Thomas and R.C. Nelson.

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

  • Heat transfer in a complex trailing edge passage for a high pressure turbine blade. Pt. 2, Simulation results [microform] / David L. Rigby, Ronald S. Bunker.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS51556

  • Predicting modes of the unsteady vorticity field near the trailing edge of a blade [microform] / William J. Devenport and Nicolas Spitz.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55154

  • NACA 0015 wing pressure and trailing vortex measurements [microform] / K.W. McAlister and R.K. Takahashi.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS62410

  • Trailing edge flow conditions as a factor in airfoil design [microform] / by A. I. Ormsbee and Mark D. Maughmer.

    • Text
    • Urbana, Ill. : Aeronautical and Astronautical Engineering Dept., University of Illinois ; [Washington, DC : National Aeronautics and Space Administration, 1984]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS86754

  • Reduction of the shock wave intensity by modifying the transsonic [i.e. transonic] blade trailing edge [microform] / Piotr Doerffer.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1983]
    • 1983

  • Calculation of transonic flow in a linear cascade [microform] / Leo F. Donovan.

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

  • 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

  • Rapid state space modeling tool for rectangular wing aeroservoelastic studies / Peter M. Suh, Howard J. Conyers, Dimitri N. Mavris.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Armstrong Flight Research Center, September 2015.
    • 2015-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65159

  • Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf / Milton Lamb and John G. Taylor, Mark C. Frassinelli.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 1996.
    • 1996-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65363

  • A model for jet-surface interaction noise using physically realizable upstream turbulence conditions / Mohammed Z. Afsar, Stewart J. Leib, Richard F. Bozak.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo65869

  • The transition from thick to thin plate wake physics : whither vortex shedding? / Man Mohan Rai.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, March 2016.
    • 2016-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo68595

  • Flat plate wake velocity statistics obtained with circular and elliptic trailing edges / Man Mohan Rai.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, August 2016.
    • 2016-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo73018

  • Intermittency and cessation of vortex shedding in the wake of a thin flat plate with a circular trailing edge / Man Mohan Rai.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, August 2018.
    • 2018-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo111056

  • Jet surface interaction, scrubbing noise / Abbas Khavaran.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2013.
    • 2013-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53507

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