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  • An experimental study of turbulent skin friction reduction in supersonic flow using a microblowing technique [microform] / Danny P. Hwang.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : Available from National Technical Information Service, [1999]
    • 1999

  • 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

  • An analysis code for the Rapid Engineering Estimation of Momentum and Energy Losses (REMEL) [microform] / Lawrence J. DeChant.

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

  • Reflection type skin friction meter [microform] / inventors, Promode R. Bandyopadhyay, Leonard M. Weinstein.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows [microform] / Khaled S. Abdol-Hamid, B. Lakshmanan, John R. Carlson.

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

  • 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

  • Development of a new instrument for direct skin friction measurements [microform] : final report for NASA grant NAG 1-303 / by A.D. Vakili, J.M. Wu.

    • Text
    • Tullahoma, TN : Gas Dynamics Division, The University of Tennessee Space Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Fiber optic pressure sensors in skin-friction measurements [microform] : final report / Robert Kidwell.

    • Text
    • Kingston, R.I. : University of Rhode Island, Dept. of Physics ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • 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

  • Shock tunnel studies of scramjet phenomena 1994. Supplements 11 and 12 [microform].

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

  • Instrumentation development for study of Reynolds analogy in reacting flows [microform] / D.J. DeTurris.

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

  • A proof of concept experiment for reducing skin friction by using a micro-blowing technique [microform] / Danny P. Hwang.

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

  • Shock tunnel studies of scramjet phenomena 1995. Supplement 13 [microform] / R.G. Morgan, R.J. Stalker, and A. Paull.

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

  • Wing leading edge joint laminar flow tests [microform] / Aaron Drake ... [et al.].

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

  • Computational study of surface tension and wall adhesion effects on an oil film flow underneath an air boundary layer [microform] / Alan Celić, Gregory G. Zilliac.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Further developments of the fringe-imaging skin friction technique [microform] / Gregory G. Zilliac.

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

  • Development of in-fiber reflective Bragg gratings as shear stress monitors in aerodynamic facilities [microform] / Devendra S. Parmar, Danny R. Sprinkle and Jag J. Singh.

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

  • Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction [microform] : 32nd Aerospace Sciences Meeting & Exhibit, January 10-13, 1994/Reno, NV / by Jeffrey K. Wideman ... [et al.].

    • Text
    • Washington, D.C. : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Real-time method for estimating viscous forebody drag coefficients [microform] / Stephen A. Whitemore ... [et al.].

    • 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, 2000]
    • 2000

  • Effectiveness of micro-blowing technique in adverse pressure gradients [microform] / Gerard E. Welch ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [2001]
    • 2001

  • Shock tunnel studies of scramjet phenomena 1994 [microform] : supplements 11 and 12 / R.G. Morgan, A. Paull, and R.J. Stalker.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1997]
    • 1997

  • Hydrodynamic aspects of shark scales [microform] / William G. Rashi, John A. Musick.

    • 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

  • Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport [microform] / Milton Lamb and William K. Abeyounis.

    • 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

  • Enhanced viscous flow drag reduction using acoustic excitation : final report / R. T. Nagel.

    • Text
    • Hampton, Va. : NASA Langley Research Center, [1988?]
    • 1988
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS112051

  • Enhanced viscous flow drag reduction using acoustic excitation [microform] : final report / R. T. Nagel.

    • Text
    • Hampton, Va. : NASA Langley Research Center, [1988?]
    • 1988
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS112051

  • Wing leading edge joint laminar flow tests / Aaron Drake [and four others].

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, October 1996.
    • 1996-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65484

  • A proof of concept experiment for reducing skin friction by using a micro-blowing technique / Danny P. Hwang.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, October 1996.
    • 1996-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70082

  • Effectiveness of micro-blowing technique in adverse pressure gradients / Gerard E. Welch [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center : U.S. Army Research Laboratory, January 2001.
    • 2001-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo86659

  • Experimental evaluation of the penalty associated with micro-blowing for reducing skin friction / Danny P. Hwang and Tom J. Biesiadny.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, December 1997.
    • 1997-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo174885

  • Viscous drag reduction in boundary layers / edited by Dennis M. Bushnell, Jerry N. Hefner.

    • Text
    • Washington, DC : American Institute of Aeronautics and Astronautics, ©1990.
    • 1990
    • 1 Item
    FormatCall NumberItem Location
    Text TL574.D7 V58 1990Off-site

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