Online Books by
Charles F. Whitcomb
Books from the extended shelves:
Whitcomb, Charles F.: Air-flow and power characteristics of the Langley 16-foot transonic tunnel with slotted test section / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), also by Vernon G. Ward, Merwin D. Pearson, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Whitcomb, Charles F.: An investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30 degree swepptback wing at transonic speeds (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), also by Chris C. Critzos, Philippa F. Brown, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Whitcomb, Charles F.: Static stability and control characteristics of two large-dihedral right triangular pyramid lifting reentry configurations at a mach number of 3.05 / (Washington, D.C. : National Aeronautics and Space Administration, 1960), also by Willard E. Foss and Langley Research Center (page images at HathiTrust)
Whitcomb, Charles F.: Subsonic and transonic pressure distributions around a bluff afterbody in the wake of a 120⁰ cone for various separation distances / (Washington : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1971), also by James Wayne Sawyer and United States National Aeronautics and Space Administration (page images at HathiTrust)
Whitcomb, Charles F.: Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]), also by Harry T. Norton and United States National Aeronautics and Space Administration (page images at HathiTrust)
Whitcomb, Charles F.: Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches /, also by Harry T. Norton, Langley Aeronautical Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
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