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  • Low speed analysis of mission adaptive flaps on a high speed civil transport configuration [microform] / Victor R. Lessard.

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

  • Control of low-speed turbulent separated flow over a backward-facing ramp [microform] / by John C. Lin.

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

  • Response of composite materials to low velocity impact [microform] / K. Srinivasan, W.C. Jackson and J.A. Hinkley.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [St. Louis, Mo.] : US Army Aviation Systems Command, Aviation R&T Activity ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • A prediction of 3-D viscous flow and performance of the NASA low-speed centrifugal compressor [microform] / John Moore, Joan G. Moore.

    • Text
    • Blacksburg, Va. : Mechanical Engineering Dept., Virginia Polytechnic Institute and State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • NASA low-speed axial compressor for fundamental research [microform] / Charles A. Wasserbauer, Harold F. Weaver, Richard G. Senyitko.

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

  • Helicopter low-speed yaw control [microform] / inventors, John C. Wilson, Henry L. Kelley, Cynthia A. Crowell.

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

  • Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system [microform] / Daniel W. Banks and John W. Paulson.

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

  • NASA low-speed axial compressor for fundamental research [microform] / Charles A. Wasserbauer, Harold F. Weaver, Richard G. Senyitko.

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

  • Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50̊ [microform] / Scott P. Fears, Holly M. Ross, and Thomas M. Moul.

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

  • Evaluation of the impact response of textile composites [microform] / M.A. Portanova.

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

  • Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes [microform] / Gregory M. Catlin, Brian E. McGrath.

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

  • A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region [microform] / Edward C. Polhamus.

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

  • Preconditioning methods for low-speed flows [microform] / E. Turkel, V.N. Vatsa, R. Radespiel.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Effects of stator indexing on performance in a low speed multistage axial compressor [microform] / Wendy S. Barankiewicz and Michael D. Hathaway.

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

  • Planetary and primitive object strength measurements and sampling apparatus [microform] : NASA #NAGW 2439, final report; February 1, 1991 through January 31, 1997 / Thomas J. Ahrens, principal investigator.

    • Text
    • Pasadena, Calif. : California Institute of Technology, Seismological Laboratory ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept [microform] / David E. Hahne.

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

  • Low speed aerodynamics of the X-38 CRV [microform] : summary of research NAG9-927, 5/97-4/98 / Komerath, N.M. ... [et al.].

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

  • Numerical speed of sound and its application to schemes for all speeds [microform] / Meng-Sing Liou, Jack R. Edwards.

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

  • Effect of speed (centrifugal load) on gear crack propagation direction [microform] / David G. Lewicki.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS23200

  • Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets [microform] / Charles J. Trefny and Joseph W. Wasserbauer.

    • 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

  • Summary of a study to determine low-velocity impact damage and residual tension strength for a thick graphite/epoxy motor case [microform] / C.C. Poe, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS58426

  • Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70̊ / Holly M. Ross, Scott P. Fears, and Thomas M. Moul.

    • 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/LPS60753

  • 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

  • Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil [microform] / David E. Hahne and Frank L. Jordan, Jr.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67812

  • Effects of leading-edge devices on the low-speed aerodynamic characteristics of a highly-swept arrow-wing [microform] / Samuel J. Scott, Oran W. Nicks, and P. K. Imbrie.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • Fundamental studies of low velocity impact resistance of graphite fiber reinforced polymer matrix composites [microform] / Kenneth J. Bowles.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1985]
    • 1985

  • An aerodynamic analysis computer program and design notes for low speed wing flap systems [microform] / Harry W. Carlson and Kenneth B. Walkley ; prepared for Langley Research Center under contract NAS1-16000.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1983.
    • 1983
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS104929

  • A comparison of quasi-static indentation to low-velocity impact / A. T. Nettles, M. J. Douglas.

    • Text
    • [Marshall Space Flight Center, AL] : National Aeronautics and Space Administration, Marshall Space Flight Center, [2000]
    • 2000
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo33154

  • A comparison of quasi-static indentation to low-velocity impact [microform] / A. T. Nettles, M. J. Douglas.

    • Text
    • [Marshall Space Flight Center, AL] : National Aeronautics and Space Administration, Marshall Space Flight Center, [2000]
    • 2000

  • Low velocity instrumented impact testing of four new damage tolerant carbon/epoxy composite systems / D.G. Lance and A.T. Nettles.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, VA : For sale by the National Technical Information Service, 1990.
    • 1990
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS60878

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