The Online Books Page

Books by Charles E. Mercer:

Books in the extended shelves:

• Mercer, Charles E.: The Drummond tradition. (Putnam, 1957) (page images at HathiTrust; US access only)
• Mercer, Charles E.: Effect of afterbody ejection configurations on the performance at transonic speeds of a pylon-supported Nacelle model having a hot-jet exhaust (National Aeronautics and Space Administration :, 1962), also by John M. Swihart, Harry T. Norton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Mercer, Charles E.: Effect of afterbody terminal fairings on the performance of a pylon-mounted turbojet-nacelle model (National Aeronautics and Space Administration, 1960), also by Conrad M. Willis and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Mercer, Charles E.: Effect of geometric parameters on the static performance of an annular nozzle with a concave central base (National Aeronautics and Space Administration :, 1962), also by Albert J. Simonson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Mercer, Charles E.: Effects of nozzle interfairing modifications on longitudinal aerodynamic characteristics of a twin-jet, variable-wing-sweep fighter model (National Aeronautics and Space Administration ;, 1975), also by David E. Reubush and Langley Research Center (page images at HathiTrust)
• Mercer, Charles E.: Exhaust-nozzle characteristics for a twin-jet variable-wing-sweep fighter airplane model at Mach numbers to 2.2 (National Aeronautics and Space Administration ;, 1974), also by David E. Reubush and Langley Research Center (page images at HathiTrust)
• Mercer, Charles E.: Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Michael J. Mann and Langley Research Center (page images at HathiTrust)
• Mercer, Charles E.: Investigation at transonic speeds of a fixed divergent ejector installed in a single-engine fighter model (National Advisory Committee for Aeronautics, 1958), also by John M. Swihart, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Mercer, Charles E.: Investigation of effect of propulsion system installation and operation on aerodynamics of an airbreathing hypersonic airplane at Mach O.3 to 1.2 (National Aeronautics and Space Administration ;, 1977), also by James M. Cubbage, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Mercer, Charles E.: It's all in the game (Putnam, 1960), also by James J. Shea (page images at HathiTrust)
• Mercer, Charles E.: NASA TN D-5655 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), also by Bobby L. Berrier, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Mercer, Charles E.: Performance characteristics of a single-engine fighter model fitted with an in-flight thrust reverser (National Aeronautics and Space Administration, 1971), also by Donald L. Maiden, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Mercer, Charles E.: Performance characteristics of an isolated coannular plug nozzle at transonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by James R. Burley and Langley Research Center (page images at HathiTrust)
• Mercer, Charles E.: Pilgrim strangers, a novel. (Putnam, 1961) (page images at HathiTrust; US access only)
• Mercer, Charles E.: Static thrust of an annular nozzle with a concave central base (National Aeronautics and Space Administration :, 1960), also by Blake W. Corson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Mercer, Charles E.: Supercritical maneuvering fighter configuration : wind-tunnel investigation at Mach numbers of 0.60 to 0.95 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Michael J. Mann, Richard L. Campbell, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Mercer, Charles E.: There comes a time. (Putnam, 1955) (page images at HathiTrust)
• Mercer, Charles E.: Transonic aerodynamic characteristics of a supersonic cruise aircraft research model with the engines suspended above the wing (National Aeronautics and Space Administration, 1979), also by George T. Carson (page images at HathiTrust; US access only)
• Mercer, Charles E.: Transonic off-design performance of a fixed divergent ejector designed for a mach number of 2.0 (National Aeronautics and Space Administration, 1959), also by Harry T. Norton, Marlowe D. Cassetti, and United States National Aeronautics and Space Administration (page images at HathiTrust)

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