Research Catalog

  • Duct flow nonuniformities for space shuttle main engine (SSME) [microform] : final report / by Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center.

    • Text
    • Marshall Space Flight Center, AL : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988
  • Numerical simulation of the flow about the F-18 HARV at high angle of attack [microform] / Scott M. Murman.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • BladeCAD, an interactive geometric design tool for turbomachinery blades [microform] / Perry L. Miller ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Three-dimensional Navier-Stokes analysis and redesign of an imbedded bellmouth nozzle in a turbine cascade inlet section [microform] / P.W. Giel ... [et al.].

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Flow boiling enhancement for thermal management systems [microform] : final report : from the Thermal Science Research Center (TSRC) / by Ronald D. Boyd [principal investigator].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Bubble generation in a continuous liquid flow under gravity conditions [microform] / Salvatore Cezar Pais.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999
  • Acoustic reflection and transmission of 2-dimensional rotors and stators, including mode and frequency scattering effects [microform] / Donald B. Hanson.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999
  • Effect of jet injection angle and number of jets on mixing and emissions from a reacting crossflow at atmospheric pressure [microform] / D. St. John and G. S. Samuelsen.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [2000]
    • 2000
  • Flows in pinned arrays simulating brush seals [microform] / R.C. Hendricks ... [et al.].

    • Text
    • [Cleveland, Ohio? : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, Va. : For sale by the National Technical Information Service, 1996]
    • 1996
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60620
  • An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct [microform] / B. A. Reichert and W. R. Hingst, and T. H. Okiishi.

    • Text
    • [Cleveland, Ohio : Lewis Research Center, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS62060
  • Analytical study of the origin and behavior of asymmetric vortices [microform] / Murray Tobak, David Degani, Gregory G. Zilliac.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67462
  • A knowledge-based approach to automated flow-field zoning for computational fluid dynamics [microform] / Alison Andrews Vogel.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS70935
  • Reduction of the shock wave intensity by modifying the transsonic [i.e. transonic] blade trailing edge [microform] / Piotr Doerffer.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1983]
    • 1983
  • BladeCAD : an interactive geometric design tool for turbomachinery blades / Perry L. Miller IV [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, July 1996.
    • 1996-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo69229
  • Flows in pinned arrays simulating brush seals / R.C. Hendricks [and three others].

    • Text
    • Cleveland, Ohio : National National Aeronautics and Space Administration, Lewis Research Center, December 1996.
    • 1996-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70383
  • Effects of forebody geometry on subsonic boundary-layer stability / S. S. Dodbele.

    • 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/LPS60902

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