The Online Books Page

Online Books by

Ivan E. Beckwith

Books from the extended shelves:

• Beckwith, Ivan E.: Application of similar solutions to calculation of laminar heat transfer on bodies with yaw and large pressure gradient in high-speed flow (National Aeronautics and Space Administration :, 1961), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Beckwith, Ivan E.: The compressible turbulent boundary layer on a blunt swept slab with and without leading-edge blowing (National Aeronautics and Space Administration ;, 1971), also by James L. Hunt, Dennis M. Bushnell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Beckwith, Ivan E.: Correlations of supersonic boundary-layer transition on cones including effects of large axial variations in wind-tunnel noise (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by Fang-Jenq Chen, Theodore R. Creel, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Beckwith, Ivan E.: Effects of a modified leading edge on noise and boundary-layer transition in a rod-wall sound shield at mach 5 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Theodore R. Creel, W. E. Zorumski, Barbara B. Holley, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Beckwith, Ivan E.: Free-stream noise and transition measurements on a cone in a Mach 3.5 pilot low-disturbance tunnel (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 (page images at HathiTrust)
• Beckwith, Ivan E.: Görtler vortices and transition in wall boundary layers of two Mach 5 nozzles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Barbara B. Holley, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Beckwith, Ivan E.: Local heat transfer and recovery temperatures on a yawed cylinder at a mach number of 4.15 and high Reynolds numbers (G.P.O., 1961), also by James J. Gallagher (page images at HathiTrust)
• Beckwith, Ivan E.: NASA TN D-5496 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by William D. Harvey, Dennis M. Bushnell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Beckwith, Ivan E.: NASA TN D-6192 (National Aeronautics and Space Administration ;, 1971), also by Frank L. Clark, William D. Harvey, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Beckwith, Ivan E.: Noise reduction in a Mach 5 wind tunnel with a rectangular rod-wall sound shield (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by Theodore R. Creel, J. Wayne Keyes, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Beckwith, Ivan E.: Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Theodore R. Creel, Fang-Jenq Chen, and Langley Research Center (page images at HathiTrust)
• Beckwith, Ivan E.: Similar solutions for the compressible boundary layer on a yawed cylinder with transpiration cooling (Langley Research Center ;, 1959), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Beckwith, Ivan E.: Similarity solutions for small cross flows in laminar compressible boundary layers (U.S. G.P.O.], 1961) (page images at HathiTrust)

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