Search results for: Moffitt, Thomas P.
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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], 1983Physical Description: 16 pages : illustrations ; 28 cm.Holdings: Loading…
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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, 1981Physical Description: 1 online resource (12 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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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], 1980Other Authors: “…Moffitt, Thomas P.…”
Physical Description: 15 pages : illustrations ; 28 cm.Holdings: Loading…
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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.Other Authors: “…Moffitt, Thomas P.…”
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981
Physical Description: 12 pages : illustrations ; 27 cm.Holdings: Loading…
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5
Incidence loss for fan turbine rotor blade in two-dimensional cascade
Authors: Kline, John F.Other 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: 8 pages : illustrations ; 28 cm.Holdings: Loading…
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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.Other Authors:
Published: National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978Physical Description: 46 pages : illustrations ; 27 cm.Holdings: Loading…
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7
Performance of a high-work, low-aspect-ratio turbine tested with a realistic inlet radial temperature profile
Authors: Stabe, Roy G.Other Authors:
Published: [National Aeronautics and Space Administration], 1984Physical 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.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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