More about Thomas J. King:
| | Books by Thomas J. King: Books in the extended shelves: King, Thomas J.: Aerodynamic characteristics of a wing with quarter-chord line swept back 45 degrees, aspect ratio 4, taper ratio 0.3, and NACA 65A006 airfoil section. Transonic-bump method (National Advisory Committee for Aeronautics, 1949), also by Boyd C. Myers, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) King, Thomas J.: 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, H. Norman Silvers, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) King, Thomas J.: Some effects of tail height and wing plan form on the static longitudinal stability characteristics of a small-scale model at high subsonic speeds (National Advisory Committee for Aeronautics, 1954), also by Albert G. Few, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
Find more by Thomas J. King at your library, or elsewhere.
|