Books by Joseph F. Wasserbauer:
Books in the extended shelves:
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Wasserbauer, Joseph F.: Boundary-layer bleed system study for a full-scale, mixed-compression inlet with 45 percent internal contraction (U.S. National Aeronautics and Space Administration ;, 1976), also by Robert J. Shaw, Harvey E. Neumann, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)- Wasserbauer, Joseph F.: Design of a very-low-bleed Mach 2.5 mixed-compression inlet with 45 percent internal contraction (National Aeronautics and Space Administration ;, 1975), also by Harvey E. Neumann, Robert J. Shaw, and Lewis Research Center (page images at HathiTrust)
- Wasserbauer, Joseph F.: Distortion in a full-scale bicone inlet with internal focused compression and 45 percent internal contraction (National Aeronautics and Space Administration ;, 1974), also by Robert J. Shaw, Harvey E. Neumann, and Lewis Research Center (page images at HathiTrust)
- Wasserbauer, Joseph F.: Field-enhanced thermionic emission from electrodes of cesium ion thrustor (National Aeronautics and Space Administration :, 1965), also by Lewis Research Center (page images at HathiTrust)
- Wasserbauer, Joseph F.: NASA TN D-5338 (National Aeronautics and Space Administration ;, 1969), also by Lewis Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Wasserbauer, Joseph F.: Performance and surge limits of a TF30-P-3 turbofan engine/axisymmetric mixed-compression inlet propulsion system at Mach 2.5 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Robert J. Shaw, Harvey E. Neumann, and Lewis Research Center (page images at HathiTrust)
- Wasserbauer, Joseph F.: Performance of small (100-lb thrust) rockets motors using coaxial injection of hydrazine and nitrogen tetroxide (National Aeronautics and Space Administration :, 1961), also by William Tabata and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Wasserbauer, Joseph F.: Performance of vortex generators in a Mach 2.5 low-bleed full-scale 45-percent-internal-contraction axisymmetric inlet (National Aeronautics and Space Administration ;, 1975), also by Harvey E. Neumann, Robert J. Shaw, and Lewis Research Center (page images at HathiTrust)
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