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Blunt bodies

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• Theoretical flow field calculations for project ram / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by H. Webb, North American Rockwell Corporation, and Langley Research Center (page images at HathiTrust)
• Effects of nose bluntness, fineness ratio, cone angle, and model base on the static aerodynamic characteristics of blunt bodies at Mach numbers of 1.57, 1.80, and 2.16 and angles of attack up to 180 ̊/ (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 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)
• Effect of localized mass transfer near the stagnation region of blunt bodies in hypersonic flight / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Paul M. Chung and Ames Research Center (page images at HathiTrust)
• Effect of ablation product absorption and line transitions on shock layer radiative transport / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 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 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 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 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969), by Y. S. Chou, Lockheed Missles & Space Company, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Radiative coupled viscous flow with massive blowing / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1973), by Y. S. Chou, Ames Research Center, and Lockheed Missiles and Space Company (page images at HathiTrust)
• Shielding of partially reflecting stagnation surfaces against radiation by transpiration of an absorbing gas / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Supt. of Docs., U.S. G.P.O., Washington 25, D.C. 22151], 1961), by John Thomas Howe and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Flow-field investigation for large-angle cones with short spikes at a Mach number of 9.6 / (Washington, D.C. : 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)
• Experimental investigation of magnetoaerodynamic flow around blunt bodies / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by S. Kranc, A. B. Cambel, M. C. Yuen, and Ill.) Northwestern University (Evanston (page images at HathiTrust)
• Aerodynamic effects of bulbous bases / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by Lars E. Ericsson, J. Peter Reding, Lockheed Missiles and Space Company, and Langley Research Center (page images at HathiTrust)
• Free flight observation of a separated turbulent flow including heat transfer up to Mach 8.5 / (Washington, [D.C.] : 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 / (Washington, [D.C.] : 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 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Maxime A. Faget, James J. Buglia, Benjamine J. Garland, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An approximate method for calculating surface pressures on curved profile blunt plates in hypersonic flow / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Marcus O. Creager and Ames Research Center (page images at HathiTrust)
• Aerodynamic investigation of sharp cone-cylinder spikes on 120 ̊blunted cones at Mach numbers of 3.00, 4.50, and 6.00 / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1969), by Robert J. McGhee, W. Frank Staylor, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A time-dependent method for calculating supersonic blunt-body flow fields with sharp corners and embedded shock waves / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Richard W. Barnwell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental investigation of boundary-layer transition on a 10 ̊half-angle cone at Mach 6.9 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Michael C. Fischer, 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 / (Washington, [D.C.] : 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 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by John T. Howe, William A. Mersman, and Ames Research Center (page images at HathiTrust)
• Blunt-body stagnation-region flow with nongray radiation heat transfer : a singular perturbation solution / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by Walter B. Olstad, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Exploratory investigation of the effect of a forward-facing jet on the bow shock of a blunt body in a Mach number 6 free stream / (Washington, D.C. : 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; US access only)
• Stagnation-point solutions for inviscid radiating shock layers / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 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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