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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

  • The interactions of a flame and its self-induced boundary layer [microform] / James D. Ott and Elaine S. Oran, John D. Anderson.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Textbook multigrid efficiency for the incompressible Navier-Stokes equations [microform] : high Reynolds number wakes and boundary layers / James L. Thomas, Boris Diskin, Achi Brandt.

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

  • Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions [microform] / Kamlesh Kapoor, Bernard H. Anderson.

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

  • Analysis and evaluation of an integrated laminar flow control propulsion system [microform] : final technical report / Theo G. Keith, Jr., Kenneth J. De Witt.

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

  • User's manual for the Langley boundary layer noise propagation program (MRS-BLP) [microform] / Peter L. Spence.

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

  • Instabilities originating from suction holes used for laminar flow control (LFC) [microform] / Jonathan H. Watmuff.

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

  • 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

  • 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

  • Acoustic receptivity due to weak surface inhomogeneities in adverse pressure gradient boundary layers [microform] / Meelan Choudhari, Lian Ng, and Craig Streett.

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

  • Task A, flow energizers progress report [microform] / D. Ward ... [et al.].

    • Text
    • College Station, TX : Aerospaced [sic] Engineering Dept., Texas A&M University ; Hampton, Va. : [National Aeronautics and Space Administration], Langley Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1987?]
    • 1987

  • Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research [microform] : final report / Steven P. Schneider.

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

  • Parametric study on laminar flow for finite wings at supersonic speeds [microform] / Joseph Avila Garcia.

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

  • Application of hybrid laminar flow control to global range military transport aircraft [microform] / Roy H. Lange.

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

  • 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

  • LFC leading edge glove flight [microform] : aircraft modification design, test article development, and systems integration / F.R. Etchberger, et al.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1983]
    • 1983

  • Stability characteristics of a supersonic boundary layer and their relation to the position of the laminar-turbulent transition point [microform] / V.I. Lysenko.

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

  • Numerical simulations of the flow in the HYPULSE expansion tube [microform] / Gregory J. Wilson, Myles A. Sussman, and Robert J. Bakos.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames 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

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

    • Text
    • Moffett Field, CA : Ames 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

  • 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

  • An approach to the constrained design of natural laminar flow airfoils [microform] : a thesis ... / by Bradford Earl Green.

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

  • 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

  • An approach to the constrained design of natural laminar flow airfoils [microform] / Bradford E. Green.

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

  • Combustion of solid fuel slabs with gaseous oxygen in a hybrid motor analog [microform] / Martin J. Chiaverini ... [et al.].

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

  • 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

  • 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

  • Instability and transition of flow at, and near, an attachment-line [microform] : including control by surface suction / A. Smith and D.I.A. Poll.

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

  • Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions [microform] / William A. Wood.

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

  • Overview of laminar flow control [microform] / Ronald D. Joslin.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • High Reynolds number hybrid laminar flow control (HLFC) flight experiment. IV, Suction system design and manufacture [microform] / Boeing Commercial Airplane Group.

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

  • High Reynolds number hybrid laminar flow control (HLFC) flight experiment. III, Leading edge design, fabrication, and installation [microform] / Boeing Commercial Airplane Group.

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

  • High Reynolds number hybrid laminar flow control (HLFC) flight experiment. II, Aerodynamic design [microform] / Boeing Commercial Airplane Group.

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

  • Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment [microform] / Laurie A. Marshall.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Hanover, MD : NASA Center for AeroSpace Information [distributor] ; Springfield, VA : National Technical Information Service [distributor, 1999]
    • 1999

  • Aerothermal tests of a 12.5⁰ cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes [microform] / Robert J. Nowak, Cindy W. Albertson, and L. Roane Hunt.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
    • 1985

  • The unsteady laminar boundary layer on an axisymmetric body subject to small amplitude fluctuations in the free-stream velocity [microform] / Peter W. Duck.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS59768

  • A review of high-speed, convective, heat-transfer computation methods [microform] / Michael E. Tauber.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60002

  • Mach 10 experimental database of a three-dimensional scramjet inlet flow field [microform] / Scott D. Holland.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, VA : Available from the National Technical Information Service, 1995]
    • 1995
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60779

  • Interactive calculation procedures for mixed compression inlets [microform] / Eli Reshotko.

    • Text
    • Cleveland, Ohio : Dept. of Mechanical and Aerospace Engineering, School of Engineering, Case Institute of Technology, Case Western Reserve University, [1983]
    • 1983
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60916

  • Simulation of glancing shock wave and boundary layer interaction [microform] / Ching-Mao Hung.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS73542

  • Stability of the laminar boundary layer in a streamwise corner [microform] / by William D. Lakin.

    • Text
    • Norfolk, Va. : Old Dominion University Research Foundation ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

  • Numerical approach for the aerodynamic analysis of airfoils with laminar separation [microform] / prepared by David W. Halt and Dean R. Bristow.

    • Text
    • St. Louis, Mo. : McDonnel Douglas Corporation, McDonnel Aircraft Company ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • Structural tests and development of a laminar flow control wing surface composite chordwise joint [microform] / L. B. Lineberger.

    • Text
    • Marietta, Ga. : Lockheed-Georgia Company ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS88263

  • A flight test of laminar flow control leading-edge systems [microform] / M.C. Fischer, A.S. Wright, Jr., and R. D. Wagner.

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

  • Development of perturbations in the boundary layer [microform] / A.V. Dovgalʹ ... [et al.].

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1986]
    • 1986

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