Books by Jeffrey E. Haas:
Books in the extended shelves:
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Haas, Jeffrey E.: Analytical and experimental investigation of stator endwall contouring in a small axial-flow turbine (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by Robert J. Boyle and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)- Haas, Jeffrey E.: 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 Milton G. Kofskey and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Haas, Jeffrey E.: 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 Milton G. Kofskey and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Haas, Jeffrey E.: Cold-air performance of a tip turbine designed to drive a lift fan : II, partial admission (National Aeronautics and Space Administration ;, 1977), also by Lewis Research Center, U.S. Army Air Mobility Research and Development Laboratory, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Haas, Jeffrey E.: Cold-air performance of compressor-drive turbine of Department of Energy upgraded automobile gas turbine engine (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Richard J. Roelke, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Propulsion Laboratory (U.S.), and Lewis Research Center (page images at HathiTrust)
- Haas, Jeffrey E.: 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 Milton G. Kofskey, United States National Aeronautics and Space Administration, U.S. Army Air Mobility Research and Development Laboratory, and Lewis Research Center (page images at HathiTrust)
- Haas, Jeffrey E.: 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 Milton G. Kofskey and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
- Haas, Jeffrey E.: Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Kerry L. McLallin, Propulsion Laboratory (U.S.), Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Haas, Jeffrey E.: NASA TN D-7881 (National Aeronautics and Space Administration ;, 1975), also by Milton G. Kofskey, 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)
- Haas, Jeffrey E.: Reasons for low aerodynamic performance of 13.5-centimeter-tip-diameter aircraft engine starter turbine (National Aeronautics and Space Administration, Scientific and Technical Branch ;, 1981), also by Paul Hermann, Richard J. Roelke, Propulsion Laboratory (U.S.), and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
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