Books by Thomas P. Moffitt:
Books in the extended shelves:
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Moffitt, Thomas P.: Aerodynamic effect of a honeycomb rotor tip shroud on a 50.8-centimeter-tip-diameter core turbine (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Warren J. Whitney and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)- Moffitt, Thomas P.: Analytical investigation of cycle characteristics for advanced turboelectric space power systems (National Aeronautics and Space Administration :, 1960), also by Frederick W. Klag and Lewis Research Center (page images at HathiTrust)
- Moffitt, Thomas P.: Cold-air investigation of first state of 4 1/2-stage, fan-drive turbine with average stage-loading factor of 4.66 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Warren J. Whitney, Frank P. Behning, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Moffitt, Thomas P.: Design and cold-air test of single-stage uncooled core turbine with high work output (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Lewis Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Moffitt, Thomas P.: Design and experimental investigation of a single-stage turbine with a rotor entering relative Mach number of 2 (National Advisory Committee for Aeronautics, 1958), also by Lewis Flight Propulsion Laboratory and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
- Moffitt, Thomas P.: Effect of cooling-hole geometry on aerodynamic performance of a film-cooled turbine vane tested with cold air in a two-dimensional cascade (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by John F. Kline, Roy G. Stabe, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Moffitt, Thomas P.: Experimental investigation of partial- and full-admission characteristics of a two-stage velocity-compounded turbine (National Aeronautics and Space Administration, 1960), also by Frederick W. Klag and Lewis Research Center (page images at HathiTrust)
- Moffitt, Thomas P.: Experimental investigation of the partial- admission performance characteristics of a single-stage Mach 2 supersonic turbine (National Aeronautics and Space Administration, 1959), also by Frederick W. Klag and Langley Research Center (page images at HathiTrust)
- Moffitt, Thomas P.: Incidence loss for fan turbine rotor blade in two-dimensional cascade (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by John F. Kline, Roy G. Stabe, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
- Moffitt, Thomas P.: NASA TM X-3045 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1974), also by Wayne M. Bartlett, Herman W. Prust, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
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