The Online Books Page

Books by Walter Martin Osborn:

Books in the extended shelves:

• Osborn, Walter Martin, 1918-: Aerodynamic performance of 1.38-pressure-ratio, variable-pitch fan stage (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Royce D. Moore, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Osborn, Walter Martin, 1918-: Aerodynamic performance of a 1.35-pressure-ratio axial-flow fan stage (Natioanl Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Ronald J. Steinke, Royce D. Moore, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Osborn, Walter Martin, 1918-: 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 Laurence J. Heidelberg, George W. Lewis, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Osborn, Walter Martin, 1918-: Effect of simulated downstream flow blockage doors on the performance of an axial-flow fan rotor (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), also by Jack M. Wagner (page images at HathiTrust; US access only)
• Osborn, Walter Martin, 1918-: Effects of diffusion factor, aspect ratio, and solidity on overall performance of 14 compressor middle stages (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Werner R. Britsch, Mark R. Laessig, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Osborn, Walter Martin, 1918-: Effects of four inlet and outlet tip-annulus-area blockage configurations on the performance of an axial-flow fan rotor (National Aeronautics and Space Administration ;, 1976), also by Roy D. Hager and Lewis Research Center (page images at HathiTrust)
• Osborn, Walter Martin, 1918-: Effects of tip clearance on overall performance of transonic fan stage with and without casing treatment (National Aeronautics and Space Administration ;, 1977), also by Royce D. Moore, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Osborn, Walter Martin, 1918-: Investigation of a liquid-fluorine inducer and main-stage pump combination designed for a suction specific speed of 20000 (National Aeronautics and Space Administration ;, 1965), also by Lewis Research Center (page images at HathiTrust)
• Osborn, Walter Martin, 1918-: 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 George W. Lewis, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Osborn, Walter Martin, 1918-: 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 George W. Lewis, Royce D. Moore, and Lewis Research Center (page images at HathiTrust)
• Osborn, Walter Martin, 1918-: Performance of a 1.15-pressure-ratio axial-flow fan stage with a blade tip solidity of 0.5 (National Aeronautics and Space Administration ;, 1974), also by Ronald J. Steinke and Lewis Research Center (page images at HathiTrust)
• Osborn, Walter Martin, 1918-: 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, George W. Lewis, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Lewis Research Center (page images at HathiTrust)

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