More about H. Norman Silvers:
| | Books by H. Norman Silvers: Books in the extended shelves: Silvers, H. Norman: Effect of several tail configurations on the stability characteristics of a midwing supersonic-bomber model at mach numbers of 1.60, 1.90, 2.20, and 2.50 (National Aeronautics and Space Administration, 1960), also by R. Franklin Wells and Langley Research Center (page images at HathiTrust) Silvers, H. Norman: Experimental aerodynamic forces and moments at low speed of a missile model during simulated launching from the midsemispan location of a 45 degree sweptback wing-fuselage combination (Washington, D.C. : National Advisory Committee for Aeronautics, [1955], 1955), also by William J. Alford, Thomas J. King, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Silvers, H. Norman: Investigation of the static lateral stability and aileron characteristics of a 0.067-scale model of the Bell X-2 airplane at Mach number of 2.29, 2.78, 3.22, and 3.71 (National Advisory Committee for Aeronautics, 1958), also by Roger H. Fournier, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust) Silvers, H. Norman: Some notes on the aerodynamic loads associated with external-store installations (National Advisory Committee for Aeronautics, 1953), also by Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
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