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  • Towards understanding the mechanism of receptivity and bypass dynamics in laminar boundary layers [microform] / D.G. Lasseigne ... [et al.].

    • Text
    • Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Minnowbrook II, 1997 Workshop on Boundary Layer Transition in Turbomachines [microform] : proceedings of a workshop held at the Minnowbrook Conference Center, Syracuse University, Syracuse, New York, September 7-10, 1997 / John E. LaGraff and David E. Ashpis, editors.

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

  • Hot film wall shear instrumentation for boundary layer transition research [microform] / Steven P. Schneider.

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

  • Transonic flight test of a laminar flow leading edge with surface excrescences [microform] / Fanny A. Zuniga ... [et al.].

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

  • Laser transit anemometer measurements on a slender cone in the Langley unitary plan wind tunnel [microform] / William M. Humphreys, Jr. ... [et al.].

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

  • Analysis of the leading edge effects on the boundary layer transition [microform] : technical report, March 1, 1984 - August 31, 1990 / submitted by Pao-Liu Chow, principal investigator.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Flight survey of the 757 wing noise field and its effects on laminar boundary layer transition. Vol. I, Program description and data analysis [microform].

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

  • Flight survey of the 757 wing noise field and its effects on laminar boundary layer transition. Vol. II, Data compilation [microform].

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

  • Non-linear evolution of a second mode wave in supersonic boundary layers [microform] / Gordon Erlebacher, M.Y. Hussaini.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Experiments to verify nonparallel stability theory at Virginia Polytechnic Institute and State University, Blacksburg, Virginia [microform] : final report / by William S. Saric.

    • Text
    • Tempe, Ariz. : Dept. of Mechanical and Aerospace Engineering, Arizona State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Some characteristics of bypass transition in a heated boundary layer [microform] / K.H. Sohn, J.E. O'Brien, and E. Reshotko.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Supersonic laminar flow control research [microform] : semi-annual report #2, July 1994 - December 1994 / C.F. Lo, principal investigator.

    • Text
    • Moffett Field, CA : Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Active control of instabilities in laminar boundary-layer flow [microform] / Ronald D. Joslin, Gordon Erlebacher, M. Yousuff Hussaini.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994- ]
    • 1994-present

  • On the generation of mean flows by the interaction of Görtler vortices and Tollmien-Schlichting waves in curved channel flows [microform] / Andrew P. Bassom, Philip Hall.

    • Text
    • Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • An experimental low Reynolds number comparison of a Wortmann FX67-K170 airfoil, a NACA 0012 airfoil, and a NACA 64-210 airfoil in simulated heavy rain [microform] : final report to the NASA Langley Research Center on work accomplished under research grant NAG-1-568 / Anthony P. Craig and R. John Hansman.

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

  • Supersonic laminar flow control research [microform] : semiannual report #2 / Dr. C.F. Lo, principal investigator.

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

  • 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

  • A comparison of computer-generated lift and drag polars for a Wortman airfoil to flight and wind tunnel results [microform] : final report / principal investigators, Albion Hideto Bowers, Doral R. Sandlin.

    • Text
    • San Luis Obispo, Calif. : California Polytechnic State University, Aeronautical Engineering Dept. : [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1984]
    • 1984

  • Transitional boundary layers under the influence of high free stream turbulence, intensive wall cooling and high pressure gradinets in hot gas circulation [microform] / Klaus Rued.

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

  • Flight survey of the 757 wing noise field and its effects on laminar boundary layer transition. Vol. III, Extended data analysis [microform].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Supersonic quiet-tunnel development for laminar-turbulent transition research [microform] : final report for NASA Langley grant NAG-1-1607 / Steven P. Schneider.

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

  • Rapport d'essais du profil CAST 10 en transition dʹeclenchʹee, effectuʹes dans la soufflerie transsonique cryogʹenique T2 en pr'esence de parois auto-adaptables [microform] = Report on tests of a CAST 10 airfoil with fiexed transition in the T2 transonic cryogenic wind tunnel with self-adaptive walls / A. Seraudie, A. Blanchard, J.F. Breil.

    • Text
    • Toulouse : Centre DʹEtudes et de Recherches de Toulouse, Dept., DʹEtudes et de Recherches en Aerothermodynamique ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Feasibility study of optical boundary layer transition detection method [microform] / M. Azzazy, D. Modarress, and J.D. Trolinger.

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

  • The structure of separated flow regions occurring near the leading edge of airfoils, including transition [microform] : semi-annual status report, February 1986-July 1986 / Thomas J. Mueller, principal investigator.

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

  • Direct numerical simulation of transitional and turbulent flow over a heated flat plate using finite-difference schemes [microform] / Nateri K. Madavan.

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

  • Boundary-layer transition and global skin friction measurement with an oil-fringe imaging technique [microform] / by Daryl J. Monson, George G. Mateer, and Florian R. Menter.

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

  • Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling [microform] / Nabil M. El-Hady.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
    • 1993

  • The velocity field created by a shallow bump in a boundary layer [microform] / Michael Gaster, Chester E. Grosch, Thomas L. Jackson.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle [microform] : final report / Stephen W.D. Wolf.

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

  • A comparison of hypersonic vehicle flight and prediction results [microform] / Kenneth W. Iliff and Mary F. Shafer.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor], 1995.
    • 1995

  • Boundary layer transition studies [microform] : November 1990 to February 1995 / Jonathan H. Watmuff.

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

  • Non-linear boundary-layer receptivity due to distributed surface roughness [microform] : final report / by principal investigator, Gregory V. Selby, Tahani R. Amer, graduate research assistant.

    • Text
    • Norfolk, Va. : Old Dominion University Research Foundation, Dept. of Mechanical Engineering, College of Engineering & Technology ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • A self-contained, automated methodology for optimal flow control validated for transition delay [microform] / Ronald D. Joslin ... [et al.].

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA 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

  • Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel [microform] : final report / submitted by William S. Saric.

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

  • Simulation of crossflow instability on a supersonic highly swept wing [microform] / C. David Pruett.

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

  • Annual progress report ... entitled "an experimental investigation of the flow physics of high-lift systems" for the period March-December 1995 [microform] / by Flint O. Thomas and R.C. Nelson.

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

  • Supersonic laminar flow control research [microform] : semiannual report #4, July 1995-December 1995 / C.F. Lo, principal investigator.

    • Text
    • Moffett Field, CA : Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • The role of nonlinear critical layers in boundary layer transition [microform] / by M.E. Goldstein.

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

  • A k-E [i.e. Kappa-Epsilon] calculation of transitional boundary layers [microform] / Z. Yang and T.H. Shih.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • The effect of nonlinear critical layers on boundary layer transition [microform] / Marvin E. Goldstein.

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

  • Renormalization Group (RG) in turbulence [microform] : historical and comparative perspective / Ye Zhou, W. David McComb, George Vahala.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate) [microform] : final report of TsAGI under cooperative agreement # NCCW-72.

    • Text
    • Zhukovsky, Russia : Central Aero-Hydrodynamics Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Effect of surface waviness on transition in three-dimensional boundary-layer flow [microform] / Jamal A. Masad.

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

  • Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate) [microform] : under cooperative agreement NCC1-241 / M.N. Kogan and M.V. Ustinov.

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

  • 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

  • Instantaneous structure of turbulent separated boundary layers [microform] : report of research performed during the period August 3, 1995 to August 20, 1996, with support of grant number NAG 1 1530 / Ronald J. Adrian.

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

  • Distributed-roughness effects on stability and transition in swept-wing boundary layers [microform] : annual technical report ... NASA-Langley cooperative agreement # NCC-1-194 and the Boeing Company contract #ZA0078, during 5/17/96-12/31/96 / submitted by Ruben B. Carrillo, Jr.; Mark S. Reibert; William S. Saric (principal investigator).

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

  • Hypersonic boundary-layer transition for X-33 phase II vehicle [microform] / R.A. Thompson ... [et al.].

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

  • Measurements in transitional boundary layers under high free-stream turbulence and strong acceleration conditions [microform] : under grant NAG3-1249 / Ralph J. Volino and Terrence W. Simon.

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

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