Research Catalog

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  • Unsteady flows in a single-stage transonic axial-flow fan stator row [microform] / Michael D. Hathaway.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [St. Louis, MO] : U.S. Army Aviation Systems Command ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
    • 1986

  • Effects of shrouded stator cavity flows on multistage axial compressor aerodynamic performance [microform] / Steven R. Wellborn and Theodore H. Okiishi.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [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

  • Aeropropulsion technology (APT) [microform] : task 23--stator seal cavity flow investigation / J.J. Heidegger, E.J. Hall, and R.A. Delaney.

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

  • Benefits of swept and leaned stators for fan noise reduction [microform] / Richard P. Woodward ... [et al.].

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

  • TFaNS Ṯone ̲F̲an Ṉoise Design/Prediction ̲System [microform] / David A. Topol.

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

  • Acoustic scattering by three-dimensional stators and rotors using the SOURCE3D code [microform] / Harold D. Meyer.

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

  • Redesign and cascade tests of a supercritical controlled diffusion stator blade-section [microform] / James F. Schmidt, Thomas F. Gelder, and Leo F. Donovan.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984

  • Off-design performance loss model for radial turbines with pivoting, variable-area stators / Peter L. Meitner, Arthur J. Glassman.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980.
    • 1980-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71099

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