The Online Books Page

Books by Royce D. Moore:

Books in the extended shelves:

• Moore, Royce D.: Aerodynamic performance of 0.4066-scale model of JT8D refan stage (U.S. National Aeronautics and Space Administration ;, 1976), also by Edward R. Tysl, George Kovich, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Moore, Royce D.: Aerodynamic performance of 0.4066-scale model of JT8D refan stage with S-duct inlet (National Aeronautics and Space Administration ;, 1977), also by George W. Lewis, George Kovich, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Moore, Royce D.: Aerodynamic performance of 1.38-pressure-ratio, variable-pitch fan stage (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Walter Martin Osborn, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Moore, Royce D.: Aerodynamic performance of a 1.20-pressure-ratio fan stage designed for low noise (National Aeronautics and Space Administration ;, 1976), also by George W. Lewis, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Moore, Royce D.: Aerodynamic performance of a 1.25-pressure-ratio axial-flow fan stage (National Aeronautics and Space Administration ;, 1974), also by Ronald J. Steinke and Lewis Research Center (page images at HathiTrust)
• Moore, Royce D.: 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 Walter Martin Osborn, Ronald J. Steinke, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Moore, Royce D.: Aerodynamic performance of axial-flow fan stage operated at nine inlet guide vane angles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Lonnie Reid and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Moore, Royce D.: Design and overall performance of four highly loaded, high-speed inlet stages for an advanced high-pressure-ratio core compressor (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Lonnie Reid, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Moore, Royce D.: Detailed flow surveys of turning vanes designed for a 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Moore, Royce D.: Effect of casing treatment on overall and blade-element performance of a compressor rotor (National Aeronautics and Space Administration ;, 1971), also by Robert J. Blade, George Kovich, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Moore, Royce D.: Effect of casing treatment on overall performance of axial-flow transonic fan stage with pressure ratio of 1.75 and tip solidity of 1.5 (National Aeronautics and Space Administration ;, 1977), also by Walter M. Osborn, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Moore, Royce D.: 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, George W. Lewis, and Lewis Research Center (page images at HathiTrust)
• Moore, Royce D.: Effects of tip clearance on overall performance of transonic fan stage with and without casing treatment (National Aeronautics and Space Administration ;, 1977), also by Walter Martin Osborn, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Moore, Royce D.: Experimental evaluation of two turning vane designs for fan drive corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), also by Donald R. Boldman, Rickey J. Shyne, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Moore, Royce D.: Experimental evaluation of two turning vane designs for high-speed corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Rickey J. Shyne, Donald R. Boldman, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Moore, Royce D.: Incipient cavitation of ethylene glycol in a tunnel venturi (National Aeronautics and Space Administration :, 1965), also by Robert S. Ruggeri, Thomas F. Gelder, and Lewis Research Center (page images at HathiTrust)
• Moore, Royce D.: Incipient cavitation of Freon-114 in a tunnel venturi (National Aeronautics and Space Administration :, 1965), also by Thomas F. Gelder, Robert S. Ruggeri, and Lewis Research Center (page images at HathiTrust)
• Moore, Royce D.: Method for prediction of pump cavitation performance for various liquids, liquid temperatures, and rotative speeds (National Aeronautics and Space Administration ;, 1969), also by Robert S. Ruggeri, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Moore, Royce D.: NASA TN D-4340 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 2215], 1968), also by Thomas F. Gelder, Robert S. Ruggeri, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Moore, Royce D.: NASA TN D-4387 (National Aeronautics and Space Administration ;, 1968), also by Robert S. Ruggeri, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Moore, Royce D.: NASA TN D-4899 (National Aeronautics and Space Administration ;, 1968), also by Robert S. Ruggeri, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Moore, Royce D.: NASA TN D-5614 (National Aeronautics and Space Administration :, 1970), also by Phillip R. Meng, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Moore, Royce D.: NASA TN D-5855 (National Aeronautics and Space Administration ;, 1970), also by Phillip R. Meng, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Moore, Royce D.: NASA TN D-6361 (National Aeronautics and Space Administration :, 1971), also by Phillip R. Meng, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Moore, Royce D.: 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, Walter Martin Osborn, and Lewis Research Center (page images at HathiTrust)
• Moore, Royce D.: Performance of 1.15-pressure-ratio fan stage at several rotor blade setting angles with reverse flow (National Aeronautics and Space Administration ;, 1976), also by George Kovich and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Moore, Royce D.: Performance of a low-pressure fan stage with reverse flow (National Aeronautics and Space Administration ;, 1976), also by Edward R. Tysl, George W. Lewis, and Lewis Research Center (page images at HathiTrust)
• Moore, Royce D.: 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 Walter Martin Osborn, George W. Lewis, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Lewis Research Center (page images at HathiTrust)
• Moore, Royce D.: Performance of low-pressure ratio fan stage at two off-design blade setting (National Aeronautics and Space Administration ;, 1977), also by George Kovich, Edward R. Tysl, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Moore, Royce D.: Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.19 and 1.26, respectively, and with design pressure ratio of 2.05 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Lonnie Reid, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Lewis Research Center (page images at HathiTrust)
• Moore, Royce D.: Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.19 and 1.26, respectively, and with design pressure ration of 1.82 (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1978), also by Lonnie Reid (page images at HathiTrust)
• Moore, Royce D.: Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.78, respectively, and with design pressure ratio of 1.82 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Lonnie Reid, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Moore, Royce D.: Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.77, respectively, and with design pressure ratio of 2.05 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Lonnie Reid, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Moore, Royce D.: Rotor tip clearance effects on overall and blade-element performance of axial-flow transonic fan stage (National Aeronautics and Space Administation, Scientific and Technical Information Branch ;, 1982), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)

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