The Online Books Page

Online Books by

John S. Preisser

Books from the extended shelves:

• Preisser, John S.: Comparison of theoretical and experimental steady wing loads on a space shuttle configuration at Mach numbers of 0.6 and 1.4 (National Aeronautics and Space Administration ;, 1976), also by Harold E. Lowder and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Preisser, John S.: Flight test of a 30-foot nominal diameter disk-gap-band parachute deployed at a Mach number of 1.56 and a dynamic pressure of 11.4 pounds per square foot (National Aeronautics and Space Administration ;, 1967), also by Clinton V. Eckstrom and Langley Research Center (page images at HathiTrust)
• Preisser, John S.: Flight test of a 31.2-foot-diameter modified ringsail parachute deployed at a Mach number of 1.39 and a dynamic pressure of 11.0 pounds per square foot (National Aeronautics and Space Administration, 1967), also by Harold N. Murrow, Clinton V. Eckstrom, and Langley Research Center (page images at HathiTrust)
• Preisser, John S.: Flight test of a pure-tone acoustic source (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Arnold W. Mueller, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Preisser, John S.: Fluctuating surface pressure and acoustic radiation for subsonic normal jet impingement (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Preisser, John S.: High-altitude flight test of a reefed 12.2-meter-diameter disk-gap-band parachute with deployment at a mach number of 2.58 (National Aeronautics and Space Administration :, 1971), also by R. Bruce Grow, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Preisser, John S.: Location of noise sources using a phase-slope method (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Richard DeLoach and Langley Research Center (page images at HathiTrust)
• Preisser, John S.: Stochastic analysis of spectral broadening by a free turbulent shear layer (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Jay C. Hardin, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Preisser, John S.: Test-engine and inlet performance of an aircraft used for investigating flight effects on fan noise (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by Robert A. Golub and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)

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