The Online Books Page

Books by Charles B. Rumsey:

Books in the extended shelves:

• Rumsey, Charles B.: Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5 (National Advisory Committee for Aeronautics, 1955), also by Russell N. Hopko, Robert O. Piland, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Rumsey, Charles B.: Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration (National Advisory Committee for Aeronautics, 1955), also by Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Rumsey, Charles B.: Heat-transfer measurements in free flight at Mach numbers up to 14.6 on a flat-faced conical nose with a total angle of 29° (National Advisory Committee for Aeronautics, 1958), also by Dorothy B. Lee, United States. National Adviosry Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Rumsey, Charles B.: Heat-transfer measurements on a blunt spherical-segment nose to a Mach number of 15.1 and flight performance of the rocket-propelled model to a Mach number of 17.8 (National Aeronautics and Space Administration, 1959), also by Dorothy B. Lee and Langley Research Center (page images at HathiTrust)
• Rumsey, Charles B.: Measurements of aerodynamic heat transfer and boundary-layer transition on a 10 degree cone in free flight at supersonic mach numbers up to 5.9 (National Aeronautics and Space Administration :, 1961), also by Dorothy B. Lee and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Rumsey, Charles B.: Measurements of aerodynamic heat transfer and boundary-layer transition on a 10° cone in free flight at supersonic Mach numbers up to 5.9 (NACA, 1956), also by Dorothy B. Lee, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Rumsey, Charles B.: Measurements of aerodynamic heat transfer and boundary-layer transition on a 15⁰ cone in free flight at supersonic mach numbers up to 5.2 (National Aeronautics and Space Administration :, 1961), also by Dorothy B. Lee and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Rumsey, Charles B.: A summary of available knowledge concerning skin friction and heat transfer and its application to the design of high-speed missiles (NACA, 1951), also by Morris W. Rubesin, Steven A. Varga, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Rumsey, Charles B.: Supersonic free-flight measurements of heat transfer and transition on a 10° cone having a low temperature ratio (National Aeronautical and Space Administration, 1961), also by Charles F. Merlet, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)

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