Search results for: Moffitt, Thomas P.

Showing 1 - 7 results of 7 Refine Results
  1. 1

    Aerodynamic effect of a honeycomb rotor tip shroud on a 50.8-centimeter-tip-diameter core turbine

    Authors: Moffitt, Thomas P.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983
    Physical Description: 16 pages : illustrations ; 28 cm.
    Government Document Book
  2. 2

    Cold-air investigation of first state of 4 1/2-stage, fan-drive turbine with average stage-loading factor of 4.66

    Authors: Whitney, Warren J., Moffitt, Thomas P., Behning, Frank P.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1981
    Physical Description: 1 online resource (12 pages) : illustrations.
    Connect to online resource - All users (Federal Depository Library Program Persistant URL)
    Government Document Electronic eBook
  3. 3

    Design and cold-air test of single-stage uncooled core turbine with high work output

    Published: National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1980
    Other Authors: “…Moffitt, Thomas P.…”
    Physical Description: 15 pages : illustrations ; 28 cm.
    Government Document Book
  4. 4

    Cold-air investigation of first state of 4 1/2-stage, fan-drive turbine with average stage-loading factor of 4.66

    Authors: Whitney, Warren J.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981
    Other Authors: “…Moffitt, Thomas P.…”
    Physical Description: 12 pages : illustrations ; 27 cm.
    Government Document Microfilm Book
  5. 5

    Incidence loss for fan turbine rotor blade in two-dimensional cascade

    Authors: Kline, John F.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983
    Other Authors: “…Moffitt, Thomas P.…”
    Physical Description: 8 pages : illustrations ; 28 cm.
    Government Document Book
  6. 6

    Effect of cooling-hole geometry on aerodynamic performance of a film-cooled turbine van tested with cold air in a two-dimensional cascade

    Authors: Kline, John F.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978
    Other Authors:
    Physical Description: 46 pages : illustrations ; 27 cm.
    Government Document Book
  7. 7

    Performance of a high-work, low-aspect-ratio turbine tested with a realistic inlet radial temperature profile

    Authors: Stabe, Roy G.
    Published: [National Aeronautics and Space Administration], 1984
    Other Authors:
    Physical Description: 1 volume., Also available via Internet from the NTRS web site. Address as of 08/07/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19840016521%5F1984016521.pdf ; current access is available via PURL.
    Connect to online resource - All users (Federal Depository Library Program Persistant URL)
    Government Document Microfilm Book