Online Books by
Earl R. Keener
Books from the extended shelves:
Keener, Earl R.: Accuracy of pitot-pressure rakes for turbulent boundary-layer measurements in supersonic flow (National Aeronautics and Space Administration ;, 1971), also by Edward J. Hopkins, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
Keener, Earl R.: Airplane motions and loads induced by flying through the flow field generated by an airplane at low supersonic speeds (National Advisory Committee for Aeronautics, 1957), also by Gareth H. Jordan, Stanley P. Butchart, Flight Research Center (U.S.), United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Keener, Earl R.: Flow-separation patterns on symmetric forebodies (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986) (page images at HathiTrust)
Keener, Earl R.: NASA TN D-5544 (National Aeronautics and Space Administration :, 1969), also by Edward J. Hopkins, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Keener, Earl R.: NASA TN D-5675 (National Aeronautics and Space Administration :, 1970), also by Edward J. Hopkins, Pearl T. Louie, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Keener, Earl R.: Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing (National Aeronautics and Space Administration, 1959), also by Flight Research Center (U.S.) (page images at HathiTrust)
Keener, Earl R.: Side forces on a tangent ogive forebody with a fineness ratio of 3.5 at high angles of attack and Mach numbers from 0.1 to 0.7 (National Aeronautics and Space Administration ;, 1977), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
Keener, Earl R.: Side forces on forebodies at high angles of attack and Mach numbers from 0.1 to 0.7 : two tangent ogives, paraboloid and cone (National Aeronautics and Space Administration ;, 1977), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
Keener, Earl R.: Summary and correlation of skin-friction and heat-transfer data for a hypersonic turbulent boundary layer on simple shapes (National Aeronautics and Space Administration :, 1969), also by Edward J. Hopkins, Thomas E. Polek, George C. Mateer, Mamoru Inouye, Morris W. Rubesin, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
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