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Blunt bodies

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• Blunt bodies -- Aerodynamics
• Blunt bodies -- Effect of radiation on

• Experimental investigation of magnetoaerodynamic flow around blunt bodies (National Aeronautics and Space Administration ;, 1969), by S. Kranc, A. B. Cambel, M. C. Yuen, and Ill.) Northwestern University (Evanston (page images at HathiTrust)
• Effect of ablation product absorption and line transitions on shock layer radiative transport (National Aeronautics and Space Administration ;, 1969), by K. H. Wilson, H. Hoshizaki, Ames Research Center, Lockheed Missles & Space Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of shock precursor heating on radiative flux to blunt bodies (National Aeronautics and Space Administration ;, 1969), by L. E. Lasher, K. H. Wilson, Lockheed Missles & Space Company, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Series solution for hypersonic flow about blunt bodies (National Aeronautics and Space Administration ;, 1969), by Y. S. Chou, Lockheed Missles & Space Company, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Aerodynamic effects of bulbous bases (National Aeronautics and Space Administration ;, 1969), by Lars E. Ericsson, J. Peter Reding, Lockheed Missiles and Space Company, and Langley Research Center (page images at HathiTrust)
• Radiative coupled viscous flow with massive blowing (National Aeronautics and Space Administration ;, 1973), by Y. S. Chou, Ames Research Center, and Lockheed Missiles and Space Company (page images at HathiTrust)
• NASA TR R-295 (National Aeronautics and Space Administration ;, 1968), by Walter B. Olstad, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TR R-95 (National Aeronautics and Space Administration :, 1961), by John Thomas Howe and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• An approximate method for calculating surface pressures on curved profile blunt plates in hypersonic flow (National Aeronautics and Space Administration, 1959), by Marcus O. Creager and Ames Research Center (page images at HathiTrust)
• NASA TN D-6031 (National Aeronautics and Space Administration :, 1970), by Richard W. Barnwell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5754 (National Aeronautics and Space Administration, 1970), by W. Frank Staylor, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Free flight observation of a separated turbulent flow including heat transfer up to Mach 8.5 (National Aeronautics and Space Administration, 1960), by Dudley George McConnell and Lewis Research Center (page images at HathiTrust)
• Experimental investigation at a Mach number of 3.11 of the lift, drag, and pitching-moment characteristics of five blunt lifting bodies (National Aeronautics and Space Administration, 1960), by William Letko and Langley Research Center (page images at HathiTrust)
• Preliminary studies of manned satellites wingless configuration : nonlifting (National Aeronautics and Space Administration :, 1962), by Maxime A. Faget, James J. Buglia, Benjamine J. Garland, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of localized mass transfer near the stagnation region of blunt bodies in hypersonic flight (National Aeronautics and Space Administration, 1959), by Paul M. Chung and Ames Research Center (page images at HathiTrust)
• NASA TN D-1605 (National Aeronautics and Space Administration, 1963), by David J. Romeo, James R. Sterrett, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An approximate analysis of unsteady vaporization near the stagnation point of blunt bodies (National Aeronautics and Space Administration, 1959), by Leonard Roberts and Langley Research Center (page images at HathiTrust)
• Solutions of the laminar compressible boundary-layer equations with transpiration which are applicable to the stagnation regions of axisymmetric blunt bodies (National Aeronautics and Space Administration, 1959), by John T. Howe, William A. Mersman, and Ames Research Center (page images at HathiTrust)
• Theoretical flow field calculations for project ram (National Aeronautics and Space Administration ;, 1969), by H. Webb, North American Rockwell Corporation, and Langley Research Center (page images at HathiTrust)

• NASA TN D-5201 (National Aeronautics and Space Administration ;, 1969), by Robert J. McGhee, W. Frank Staylor, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5766 (National Aeronautics and Space Administration :, 1970), by Michael C. Fischer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-1781 (National Aeronautics and Space Administration ;, 1963), by David S. Shaw, C. Donald Babb, Dennis E. Fuller, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)

• NASA TN D-5792 (National Aeronautics and Space Administration ;, 1970), by Walter B. Olstad, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)

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