The Online Books Page

Books by William J. Nusbaum:

Books in the extended shelves:

• Nusbaum, William J.: Aerodynamic evaluation of two-stage axial-flow turbine designed for Brayton-cycle space power system (National Aeronautics and Space Administration ;, 1968), also by Milton G. Kofskey and Lewis Research Center (page images at HathiTrust)
• Nusbaum, William J.: Air-performance evaluation of a 4.0-inch-mean-diameter single-stage turbine at various inlet pressures from 0.14 to 1.88 atmospheres and corresponding Reynolds numbers from 2500 to 50,000 (National Aeronautics and Space Administration :, 1962), also by Robert Y. Wong and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Nusbaum, William J.: Cold-air investigation of prototype Snap-8 turbine (National Aeronautics and Space Administration :, 1962), also by Donald E. Holeski and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Nusbaum, William J.: Cold-air performance of free-power turbine designed for 112-kilowatt automotive gas-turbine engine : I - Design stator-vane-chord setting angle of 35 ̊ (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Milton G. Kofskey and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Nusbaum, William J.: Comparison of results of experimental and theoretical studies of blade-outlet boundary-layer characteristics of stator blade for a high subsonic Mach number turbine (National Advisory Committee for Aeronautics, 1957), also by Cavour H. Hauser, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Nusbaum, William J.: Effect of a reduction in blade thickness on performance of a single-stage 20.32-centimeter mean-diameter turbine (National Aeronautics and Space Administration ;, 1973), also by Milton G. Kofskey, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Nusbaum, William J.: Effect of stage spacing on performance of 3.75-inch-mean-diameter two-stage turbine having partial admission in the first stage (National Aeronautics and Space Administration :, 1964), also by Robert Y. Wong, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Nusbaum, William J.: Effects of specific speed on the experimental performance of a radial-inflow turbine (National Aeronautics and Space Administration ;, 1971), also by Milton G. Kofskey, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Nusbaum, William J.: Experimental investigation of a 3.0-inch-mean-diameter full-admission three-stage turbine suitable for small auxiliary power units (National Aeronautics and Space Administration :, 1965), also by Robert Y. Wong and Lewis Research Center (page images at HathiTrust)
• Nusbaum, William J.: NASA TN D-4432 (National Aeronautics and Space Administration ;, 1968), also by Milton G. Kofskey, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Nusbaum, William J.: NASA TN D-6605 (National Aeronautics and Space Administration ;, 1972), also by Milton G. Kofskey, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Nusbaum, William J.: Performance evaluation of a two-stage axial-flow turbine for two values of tip clearance (National Aeronautics and Space Administration ;, 1968), also by Milton G. Kofskey and Lewis Research Center (page images at HathiTrust)

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