Online Books by
Herman L. Bohon
Books from the extended shelves:
Bohon, Herman L.: Deployment and performance characteristics of 1.5-meter supersonic attached inflatable decelerators / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), also by Robert Miserentino, James Wayne Sawyer, and Langley Research Center (page images at HathiTrust)
Bohon, Herman L.: Deployment and performance characteristics of 5-foot-diameter (1.5 m) attached inflatable decelerators from Mach number 2.2 to 4.4 / (Washington, DC : National Aeronautics and Space Administration, 1970), also by Robert Miserentino, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Bohon, Herman L.: Drag characteristics of several towed decelerator models at Mach 3 [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), also by Robert Miserentino, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Bohon, Herman L.: Experimental investigation at mach number of 3.0 of the effects of thermal stress and buckling on the flutter of four-bay aluminum alloy panels with length-width ratios of 10 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), also by Sidney C. Dixon, George E. Griffith, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Bohon, Herman L.: Flutter design of stiffened-skin panels for hypersonic aircraft / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Walter L. Heard, Melvin S. Anderson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Bohon, Herman L.: Flutter of aerodynamically heated aluminum-alloy and stainless-steel panels with length-width ratio of 10 at mach number of 3.0 / Lawrence D. Guy and Herman L. Bohon. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), also by Lawrence D. Guy and United States National Aeronautics and Space Administration (page images at HathiTrust)
Bohon, Herman L.: Flutter of corrugation-stiffened panels at Mach 3 and comparison with theory / (Washington, D.C. : National Aeronautics and Space Administration, 1968) (page images at HathiTrust)
Bohon, Herman L.: Flutter of flat rectangular orthotropic panels with biaxial loading and arbitrary flow direction / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1963]), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
Bohon, Herman L.: Natural vibration and flutter of elastically supported corrugation-stiffened panels : experiment and theory [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 1970), also by Walter L. Heard, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Bohon, Herman L.: Panel flutter tests on full-scale X-15 lower vertical stabilizer at Mach number of 3.0 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1962), also by United States National Aeronautics and Space Administration and Langley Research Center (page images at HathiTrust)
Bohon, Herman L.: A structural merit function for aerodynamic decelerators / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), also by Melvin S. Anderson, Martin M. Mikulas, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
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