Research Catalog

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  • Flow coefficient behavior for boundary layer bleed holes and slots [microform] / B.P. Willis, D.O. Davis, and W. R. Hingst.

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

  • Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel [microform] / E.B. Plentovich and Blair B. Gloss.

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

  • The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers [microform] / E.B. Plentovich.

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

  • Mixing of multiple jets with a confined subsonic crossflow [microform]. Part II, opposed rows of orifices in rectangular ducts / James D. Holdeman, David S. Liscinsky, Daniel B. Bain.

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

  • Quick-mixing studies under reacting conditions [microform] : under grant NAG3-1110 / May Y. Leong and G.S. Samuelsen.

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

  • Optimization of jet mixing into a rich, reacting crossflow [microform] / M.Y. Leong and G.S. Samuelsen, J.D. Holdeman.

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

  • Sound absorption of a 2DOF resonant liner with negative bias flow [microform] / K.K. Ahuja, P. Cataldi, and R.J. Gaeta.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [2000]
    • 2000

  • A particle and energy balance model of the orificed hollow cathode [microform] / Matthew T. Domonkos ; prepared for the 38th Joint Propulsion Conference and Exhibit, cosponsored by the AIAA, ASME, SAE, and ASEE, Indianapolis, Indiana, July 7-10, 2002.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS42588

  • Liquid seeding atomizer [microform].

    • Text
    • [Moffett Field, Calif. : NASA Ames Research Center, 1986]
    • 1986

  • Study of orifice fabrication technologies for the liquid droplet radiator [microform] / David B. Wallace, Donald J. Hayes, and J. Michael Bush.

    • Text
    • Plano, Tex. : MicroFab Technologies, Inc. ; [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67716

  • In-flight investigation of shuttle tile pressure orifice installations [microform] / Timothy R. Moes and Robert R. Meyer, Jr.

    • 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

    http://purl.access.gpo.gov/GPO/LPS73726

  • Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the Ames unitary plan wind tunnel [microform] / Paul M. Siemers, III, Martin W. Henry.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
    • 1986

  • A particle and energy balance model of the orificed hollow cathode / Matthew T. Domonkos.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2002.
    • 2002-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS42588

  • Wind-tunnel and flight-test results for the measurements of flow variables at supersonic speeds using improved wedge and conical probes / Percy J. Bobbitt [and four others].

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37677

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