More about F. K. Moore:
| | Books by F. K. Moore: Books in the extended shelves: Moore, F. K. (Franklin K.): Acoustic propagation in a diatomic gas subject to thermal or chemical relaxation (United States Air Force, Office of Scientific Research, 1958), also by Walter E. Gibson and Cornell Aeronautical Laboratory (page images at HathiTrust) Moore, F. K. (Franklin K.): Finite-amplitude pressure waves in the radial mode of a cylinder (National Aeronautics and Space Administration ;, 1972), also by Isoroku Kubo, Lewis Research Center, and Cornell University (page images at HathiTrust) Moore, F. K. (Franklin K.): Lift hysteresis at stall as an unsteady boundary-layer phenomenon (U.S. Government Printing Office, 1956), also by United States National Advisory Committee for Aeronautics (page images at HathiTrust) Moore, F. K. (Franklin K.): NASA CR-1362 (National Aeronautics and Space Administration ;, 1969), also by Brice S. Sumner, Cornell University, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) Moore, F. K. (Franklin K.): On the viscosity of dissociated air (Buffalo, New York : Cornell University, Cornell Aeronautical Laboratory, 1961., 1961), also by United States. Air Force. Office of Scientific Research and Cornell Aeronautical Laboratory (page images at HathiTrust) Moore, F. K. (Franklin K.): The Rayleigh problem for a dissociated gas ([Buffalo, N.Y.], 1961), also by W.J. Rae and Cornell Aeronautical Laboratory (page images at HathiTrust) Moore, F. K. (Franklin K.): Research on rotating stall in axial flow compressors. Part II, On the separation of the unsteady laminar boundary layer (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), also by R. A. Hartunian, Wright Air Development Center, United States. Air Force. Air Research and Development Command, and Armed Services Technical Information Agency (U.S.) (page images at HathiTrust) Moore, F. K. (Franklin K.): A theory of rotating stall of multistage axial compressors (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Sibley School of Mechanics and Aerospace Engineering, and Lewis Research Center (page images at HathiTrust) Moore, F. K. (Franklin K.): Unsteady oblique interaction of a shock wave with a plane disturbance (National Advisory Committee for Aeronautics, 1953), also by United States National Advisory Committee for Aeronautics (page images at HathiTrust)
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