The Online Books Page

Books by George W. Lewis:

Books in the extended shelves:

• Lewis, George W., Jr: Aerodynamic performance of 0.4066-scale model of JT8D refan stage with S-duct inlet (National Aeronautics and Space Administration ;, 1977), also by Royce D. Moore, George Kovich, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lewis, George W., Jr: Aerodynamic performance of 0.5-meter-diameter, 337-meter-per-second tip speed, 1.5-pressure-ratio, single-stage fan designed for low noise aircraft engines (National Aeronautics and Space Administration ;, 1974), also by Thomas F. Gelder and Lewis Research Center (page images at HathiTrust)
• Lewis, George W., Jr: Cavitation performance of an 83 degree helical inducer operated in liquid hydrogen (National Aeronautics and Space Administration, 1961), also by D. M. Sandercock, Edward R. Tysl, and Lewis Research Center (page images at HathiTrust)
• Lewis, George W., Jr: Design and performance of a high-pressure-ratio, highly loaded axial-flow transonic compressor space (National Aeronautics and Space Administration ;, 1974), also by Edward R. Tysl, Lonnie Reid, and Lewis Research Center (page images at HathiTrust)
• Lewis, George W., Jr: Design, over-all performance and stall characteristics (National Advisory Committee for Aeronautics, 1954), also by G. K. Serovy, Francis C. Schwenk, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis, George W., Jr: Effect of casing treatment on performance of an inlet stage for a transonic multistage compressor (U.S. National Aeronautics and Space Administration ;, 1976), also by Donald C. Urasek, Royce D. Moore, and Lewis Research Center (page images at HathiTrust)
• Lewis, George W., Jr: Effect of damper on overall and blade-element performance of a compressor rotor having a tip speed of 1151 feet per second and an aspect ratio of 3.6 (National Aeronautics and Space Administration ;, 1974), also by Roy D. Hager and Lewis Research Center (page images at HathiTrust)
• Lewis, George W., Jr: Effect of several porous casing treatments on stall limit and on overall performance of an axial-flow compressor rotor (National Aeronautics and Space Administration ;, 1971), also by Walter Martin Osborn, Laurence J. Heidelberg, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Lewis, George W., Jr: NASA TN D-5506 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Walter Martin Osborn, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lewis, George W., Jr: Overall and blade-element performance of a 1.20-pressure-ratio fan stage at design blade setting angle (National Aeronautics and Space Administration ;, 1974), also by Edward R. Tysl and Lewis Research Center (page images at HathiTrust)
• Lewis, George W., Jr: Overall and blade element performance of a 1.20-pressure-ratio fan stage with rotor blades reset -5 ̊ (U.S. National Aeronautics and Space Administration ;, 1976), also by Royce D. Moore, Walter Martin Osborn, and Lewis Research Center (page images at HathiTrust)
• Lewis, George W., Jr: Overall and blade element performance of a 1.20 pressure ratio fan stage with rotor blades reset -7 ̊ (U.S. National Aeronautics and Space Administration ;, 1976), also by George Kovich and Lewis Research Center (page images at HathiTrust)
• Lewis, George W., Jr: Performance of a low-pressure fan stage with reverse flow (National Aeronautics and Space Administration ;, 1976), also by Royce D. Moore, Edward R. Tysl, and Lewis Research Center (page images at HathiTrust)
• Lewis, George W., Jr: Performance of a transonic fan stage designed for a low meridional velocity ratio (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Royce D. Moore, Walter Martin Osborn, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Lewis Research Center (page images at HathiTrust)
• Lewis, George W., Jr: Performance of inlet stage of transonic compressor (National Aeronautics and Space Administration ;, 1976), also by Donald C. Urasek, Ronald J. Steinke, and Lewis Research Center (page images at HathiTrust)

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