Research Catalog

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  • Simultaneous three-dimensional velocity and mixing measurements by use of laser Doppler velocimetry and fluorescence probes in a water tunnel [microform] / Dan H. Neuhart, David J. Wing, and Uleses C. Henderson, Jr.

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

  • Water tunnel flow visualization study of a 4.4% scale X-31 forebody [microform] / Brent R. Cobleigh and John Del Frate.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model [microform] / Stacey J. Cotton and Lisa J. Bjarke.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Development of a mulicomponent force and moment balance for water tunnel applications [microform] / Carlos J. Suárez ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
    • 1994

  • Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching [microform] / J. Moreira and H. Johari.

    • Text
    • Worcester, MA : Mechanical Engineering Dept., Worcester Polytechnic Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Water tunnel flow visualization study through poststall of 12 novel planform shapes [microform] / Gregory M. Gatlin, Dan H. Neuhart.

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

  • Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack [microform] / Brent R. Cobleigh, Mark A. Croom.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS30134

  • Feasibility of generating an "artificial" burst in a turbulent boundary layer [microform] / Mohamed Gad-el-Hak.

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

  • Water tunnel flow visualization study through poststall of 12 novel planform shapes / Gregory M. Gatlin, Dan H. Neuhart.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 1996.
    • 1996-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65353

  • Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack / Brent R. Cobleigh, Mark A. Croom.

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, May 2001.
    • 2001-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS30134

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