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  • Control of flow separation : energy conservation, operational efficiency, and safety / by Paul K. Chang.

    • Text
    • Washington : Hemisphere Pub. Cor., c1976. distributed by McGraw-Hill, [1975]
    • 1975
    • 1 Item
    FormatCall NumberItem Location
    Text JSE 77-267Offsite

  • Boundary layer and flow control, its principles and application.

    • Text
    • New York, Pergamon Press, 1961.
    • 1961
    • 2 Items
    FormatCall NumberItem Location
    Text PCP (Lachmann, G. Boundary layer and flow control) v. 1 (1961)Offsite
    FormatCall NumberItem Location
    Text PCP (Lachmann, G. Boundary layer and flow control) v. 2 (1961)Offsite

  • F-16XL-2 supersonic laminar flow control flight test experiment [microform] / Scott G. Anders and Michael C. Fischer.

    • 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

  • Subsonic investigation of a leading-edge boundary layer cont[r]ol suction system on a high-speed civil transport configuration [microform] / Bryan A. Campbell ... [et al.].

    • 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

  • Application of computational fluid dynamics to the study of vortex flow control for the management of inlet distortion [microform] / Bernhard H. Anderson and James Gibb.

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

  • Adaptive nonlinear polynomial neural networks for control of boundary layer/structural interaction [microform] / B. Eugene Parker, Jr. ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1993]
    • 1993

  • Vortex boundary-layer interactions, data report [microform] : semiannual status report on research grant no. NAGW-581, period 1 March 1985 - 31 August 1985 / P. Bradshaw, principal investigator.

    • Text
    • London : Imperial College of Science and Technology, Department of Technology ; [Springfield, Va. : For sale by the National Technical Information Service, 1985]
    • 1985

  • Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction [microform] : final report / by H.T. Nagamatsu and R. Dyer.

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

  • Acoustic receptivity of compressible boundary layers [microform] : receptivity via surface-temperature variations / Meelan Choudhari.

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

  • Effect of nonzero surface admittance on receptivity and stability of compressible boundary layer [microform] / Meelan Choudhari.

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

  • 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

  • 1989 high-speed civil transport studies [microform] / HSCT Concept Development Group, Advanced Commercial Programs, Douglas Aircraft Company.

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

  • The NASA Langley laminar-flow-control experiment on a swept supercritical airfoil [microform] : basic results for slotted configuration / Charles D. Harris ... [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], 1989.
    • 1989

  • 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

  • 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

  • Control of unsteady separated flow associated with the dynamic stall of airfoils [microform] / M.C. Wilder.

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

  • Numerical simulation of the SOFIA flowfield [microform] / Stephen P. Klotz.

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

  • On supersonic-inlet boundary-layer bleed flow [microform] / Gary J. Harloff and Gregory E. Smith.

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

  • 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

  • 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

  • Approximation of discrete-time LQG compensators for distributed systems with boundary input and unbounded measurement [microform] / J.S. Gibson, I.G. Rosen.

    • Text
    • Hampton, Va. : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 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

  • Stability and control of compressible flows over a surface with concave-convex curvature [microform] / Lucio Maestrello ... [et al.].

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Evaluation of laminar flow control systems concepts for subsonic commercial transport aircraft [microform] / McDonnel Douglas Corporation, Douglas Aircraft Company.

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

  • 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

  • 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

  • Effect of aspect ratio on sidewall boundary-layer influence in two-dimensional airfoil testing [microform] / A.V. Murthy.

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

  • Control of unsteady separated flow associated with the dynamic stall of airfoils [microform] : final report, 95-09 / M.C. Wilder.

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

  • Numerical simulation of supersonic flow using a new analytical bleed boundary condition [microform] / G.J. Harloff and G.E. Smith.

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

  • 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

  • Flow characteristics in boundary layer bleed slots with plenum [microform] / A. Hamed, J.J. Yeuan and J.D. Jun.

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

  • Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction [microform] : final report on NASA grant NAG 1-1471 for the period 01/09/93 through 01/01/95 / David S. Dolling and J.W. Barter.

    • Text
    • Austin, Tex. : Center for Aerodynamics Research, Dept. of Aerospace Engineering & Engineering Mechanics, University of Texas at Austin ; [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

  • Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction [microform] / Hyun D. Kim, Warren R. Hingst, and David O. Davis.

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

  • 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

  • Optimum suction distribution for transition control [microform] / P. Balakumar, P. Hall.

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

  • Numerical study of boundary-layer control in aerodynamics [microform] : final technical report for grant NCC 2-845, NASA-Ames Research Center; grant period: 1 January 1994 to 31 December 1995, no-cost extension to 31 December 1996 / submitted by Tom I.-P. Shih.

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

  • Porous and microporous honeycomb composites as potential boundary-layer bleed materials [microform] / D.O. Davis and B.P. Willis, M. Schoenenberger.

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

  • Supersonic laminar flow control research [microform] : NASA grant no. NAG 2-881, final report, January 1994 - June 1996 / principal investigator, Ching F. Lo; other investigators [i.e. investigator], Clark G. Wiberg.

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

  • Active control of boundary-layer instabilities [microform] : use of sensors and spectral controller / R.D. Joslin ... [et al.].

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

  • Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction [microform] / D.O. Davis, B.P. Willis, and W.R. Hingst.

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

  • Supersonic laminar flow control research [microform] : final report, July 1994-June 1996 / C.F. Lo, principal investigator.

    • Text
    • Tullahoma, TN : University of Tennessee, Space Institute ; Moffett Field, CA : Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • 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

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