The Online Books Page

Books by Milton G. Kofskey:

Books in the extended shelves:

• Kofskey, Milton G.: Aerodynamic evaluation of two-stage axial-flow turbine designed for Brayton-cycle space power system (National Aeronautics and Space Administration ;, 1968), also by William J. Nusbaum and Lewis Research Center (page images at HathiTrust)
• Kofskey, Milton G.: Cold-air performance of a 12.766-centimeter-tip aixial-flow cooled turbine (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by Jeffrey E. Haas and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Kofskey, Milton G.: Cold-air performance of a 12.766-centimeter-tip-diameter axial-flow cooled turbine : II - effect of air ejection on turbine performance (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by Jeffrey E. Haas and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Kofskey, Milton G.: Cold-air performance of a 15.41-cm-tip-diameter axial-flow power turbine with variable-area stator designed for a 75-kW automotive gas turbine engine (National Aeronautics and Space Administration ;, 1982), also by Kerry L. McLallin, Robert Y. Wong, United States. Dept. of Energy. Office of Vehicle and Engine Research and Development, and Lewis Research Center (page images at HathiTrust)
• Kofskey, Milton G.: Cold-air performance of a tip turbine designed to drive a lift fan : IV - Effect of reducing rotor tip clearance (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Jeffery E. Hass, Glen M. Hotz, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Kofskey, Milton G.: 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 William J. Nusbaum and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Kofskey, Milton G.: Comparison of secondary flows and boundary-layer accumulations in several turbine nozzles (National Advisory Committee for Aeronautics, 1953), also by Howard Z. Herzig, Hubert W. Allen, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Kofskey, Milton G.: 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 William J. Nusbaum, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Kofskey, Milton G.: Effect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanes : I--performance with coolant ejection holes plugged (U.S. National Aeronautics and Space Administration ;, 1976), also by Jeffrey E. Haas, United States National Aeronautics and Space Administration, U.S. Army Air Mobility Research and Development Laboratory, and Lewis Research Center (page images at HathiTrust)
• Kofskey, Milton G.: Effect of coolant flow ejection on aerodynamic performance of low-aspect-ratio vanes : II-performance with coolant flow ejection at temperature ratios up to 2 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by Jeffrey E. Haas and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Kofskey, Milton G.: Effects of specific speed on the experimental performance of a radial-inflow turbine (National Aeronautics and Space Administration ;, 1971), also by William J. Nusbaum, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Kofskey, Milton G.: Experimental evaluation of a 3.50-inch radial turbine designed for a 10-kilowatt space power system (National Aeronautics and Space Administration ;, 1969), also by Charles A. Wasserbauer, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Kofskey, Milton G.: Experimental investigation of loss in an annular cascade of turbine-nozzle blades of free vortex design (National Advisory Committee for Aeronautics, 1953), also by Hubert W. Allen, Richard E. Chamness, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Kofskey, Milton G.: NASA TN D-3742 (National Aeronautics and Space Administration ;, 1966), also by Lewis Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Kofskey, Milton G.: NASA TN D-4432 (National Aeronautics and Space Administration ;, 1968), also by William J. Nusbaum, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Kofskey, Milton G.: NASA TN D-6605 (National Aeronautics and Space Administration ;, 1972), also by William J. Nusbaum, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Kofskey, Milton G.: NASA TN D-7881 (National Aeronautics and Space Administration ;, 1975), also by Jeffrey E. Haas, U.S. Army Air Mobility Research and Development Laboratory, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Kofskey, Milton G.: Performance evaluation of a two-stage axial-flow turbine for two values of tip clearance (National Aeronautics and Space Administration ;, 1968), also by William J. Nusbaum and Lewis Research Center (page images at HathiTrust)
• Kofskey, Milton G.: Performance evaluation of a two-stage turbine designed for a ratio of blade speed to jet speed of 0.146 (National Aeronautics and Space Administration, 1960), also by Lewis Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Kofskey, Milton G.: Turbine for a low-cost turbojet engine (National Aeronautics and Space Administration ;, 1974), also by U.S. Army Air Mobility Research and Development Laboratory and Lewis Research Center (page images at HathiTrust)

Find more by Milton G. Kofskey at your library, or elsewhere.