More about Bernard Rashis:
| | Books by Bernard Rashis: Books in the extended shelves: Rashis, Bernard: An analytical investigation of ablation (National Aeronautics and Space Administration, 1960), also by Russell N. Hopko and Langley Research Center (page images at HathiTrust; US access only) Rashis, Bernard: An experimental investigation of ablating materials at low and high enthalpy potentials (National Aeronautics and Space Administration, 1960), also by Thomas E. Walton and United States National Aeronautics and Space Administration (page images at HathiTrust) Rashis, Bernard: Exploratory investigation of transpiration cooling of a 40 degree double wedge using nitrogen and helium as coolants at stagnation temperatures from 1,295 degrees F to 2,910 degrees F (National Aeronautics and Space Administration :, 1961), also by United States National Aeronautics and Space Administration (page images at HathiTrust) Rashis, Bernard: Exploratory investigation of transpiration cooling of a 40À double wedge using nitrogen and helium as coolants at stagnation temperatures of 1,295À to 2,910À F (NACA, 1957), also by United States National Advisory Committee for Aeronautics and Langley Aeronautical Laboratory (page images at HathiTrust) Rashis, Bernard: A Free-flight investigation of ablation of a blunt body to a mach number of 13.2 / Clyde W. Winters, William G. Witte, Bernard Rashis and Russell N. Hopko. (National Aeronautics and Space Administration :, 1962), also by Clyde W. Winters, Russell N. Hopko, William G. Witte, and United States National Aeronautics and Space Administration (page images at HathiTrust) Rashis, Bernard: Free-flight skin-temperature and surface-pressure measurements on a highly polished nose having a 100⁰ total-angle cone and a 10⁰ half-angle conical flare section up to a mach number of 4.08 (National Aeronautics and Space Administration :, 1961), also by Aleck C. Bond and United States National Aeronautics and Space Administration (page images at HathiTrust) Rashis, Bernard: Qualitative measurements of the effective heats of ablation of several materials in supersonic air jets at stagnation temperatures up to 11,000À F (NACA, 1958), also by Russell N. Hopko, William G. Witte, United States National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
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