More about Arthur Henderson:
| | Books by Arthur Henderson: Books in the extended shelves: Henderson, Arthur, 1922-: Charts for conical and two-dimensional oblique-shock flow parameters in helium at mach numbers from about 1 to 100. (National Aeronautics and Space Administration :, 1961), also by Dorothy O. Braswell and United States National Aeronautics and Space Administration (page images at HathiTrust) Henderson, Arthur, 1922-: Effect of air contamination in a helium tunnel (National Aeronautics and Space Administration, 1960), also by Frank E. Swalley and Langley Research Center (page images at HathiTrust) Henderson, Arthur, 1922-: Exploration of the solar system (National Aeronautics and Space Administration : for sale by the Supt. of Docs., U.S. Govt. Print. Off., 1974), also by AIAA Technical Committee on Space Systems, Jerry Grey, and American Institute of Aeronautics and Astronautics. Technical Committee on Space and Atmospheric Physics (page images at HathiTrust) Henderson, Arthur, 1922-: Laminar heat-transfer and pressure-distribution studies on a series of reentry nose shapes at a mach number of 19.4 in helium. (National Aeronautics and Space Administration :, 1961), also by Richard D. Wagner, W. Clint Pine, and United States National Aeronautics and Space Administration (page images at HathiTrust) Henderson, Arthur, 1922-: NASA TN D-2489 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1964), also by James P. Arrington, Roy C. Joiner, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) Henderson, Arthur, 1922-: Some aspects of air-helium simulation and hypersonic approximations (National Aeronautics and Space Administration, 1959), also by Eugene S. Love, Mitchel H. Bertram, and Langley Research Center (page images at HathiTrust) Henderson, Arthur, 1922-: Some effects of aircraft configuration on static longitudinal and directional stability characteristics at supersonic Mach numbers below 3 (National Advisory Committee for Aeronautics, 1959), also by M. Leroy Spearman and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
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