The Online Books Page

Books by Donald C. Urasek:

Books in the extended shelves:

• Urasek, Donald C.: Blade-element performance of a tandem-bladed inducer tested in water (National Aeronautics and Space Administration ;, 1969), also by Richard F. Soltis, Max J. Miller, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Urasek, Donald C.: Design and performance of a 427-meter-per-second-tip-speed two-stage fan having a 2.40 pressure ratio (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Walter S. Cunnan, William Stevans, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Urasek, Donald C.: Effect of casing treatment on performance of a two-stage high-pressure-ratio fan (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office and Lewis Research Center (page images at HathiTrust)
• Urasek, Donald C.: 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 Royce D. Moore, George W. Lewis, and Lewis Research Center (page images at HathiTrust)
• Urasek, Donald C.: Effects of increased leading-edge thickness on performance of a transonic rotor blade (National Aeronautics and Space Administration ;, 1973), also by Lonnie Reid and Lewis Research Center (page images at HathiTrust)
• Urasek, Donald C.: Effects of reset stators and a rotating, grooved stator hub on performance of a 1.92-pressure-ratio compressor stage (National Aeronautics and Space Administration ;, 1977), also by George W. Lewis, Lonnie Reid, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Urasek, Donald C.: NASA TN D-5134 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Richard F. Soltis, Max J. Miller, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Urasek, Donald C.: NASA TN D-5258 (National Aeronautics and Space Administration ;, 1969), also by Robert E. Connelly, Phillip R. Meng, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Urasek, Donald C.: Performance of inlet stage of transonic compressor (National Aeronautics and Space Administration ;, 1976), also by George W. Lewis, Ronald J. Steinke, and Lewis Research Center (page images at HathiTrust)
• Urasek, Donald C.: Performance of two-stage fan having low-aspect-ratio, first-stage rotor blading (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Walter S. Cunnan, William T. Gorrell, Propulsion Laboratory (U.S.), and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Urasek, Donald C.: Performance of two-stage fan with a first-state rotor redesigned to account for the presence of a part-span damper (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by William T. Gorrell, Propulsion Laboratory (U.S.), Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Urasek, Donald C.: Performance of two-stage fan with larger dampers on first-stage rotor (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by Lewis Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Urasek, Donald C.: Stalled and stall-free performance of axial-flow compressor stage with three inlet-guide-vane and stator-blade settings (National Aeronautics and Space Administration ;, 1977), also by Walter S. Cunnan, Ronald J. Steinke, and Lewis Research Center (page images at HathiTrust)

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