Books by William B. Igoe:
Books in the extended shelves:
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Igoe, William B.: Aerodynamic characteristics at low Reynolds numbers of several heat-exchanger configurations for wind-tunnel use (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by William G. Johnson, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)- Igoe, William B.: Calibration of the Langley 16-foot transonic tunnel with test section air removal (National Aeronautics and Space Administration ;, 1974), also by Blake W. Corson, Jack F. Runckel, and Langley Research Center (page images at HathiTrust)
- Igoe, William B.: Description of 0.186-scale model of high-speed duct of national transonic facility (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Garl L. Gentry, Dennis E. Fuller, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Igoe, William B.: Experimental investigation of oscillatory aerodynamic forces, moments and pressures acting on a tapered wing oscillating in pitch at mach numbers from 0.40 to 1.07 (National Aeronautics and Space Administration :, 1962), also by Sumner A. Leadbetter, Sherman A. Clevenson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Igoe, William B.: Flutter investigation of a true-speed dynamic model with various tip-tank configurations (National Advisory Committee for Aeronautics, 1955), also by John L. Sewall, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
- Igoe, William B.: NASA TN D-3806 (National Aeronautics and Space Administration :, 1967), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
- Igoe, William B.: Transonic aerodynamic characteristics of a wing-body combination having a 52.2⁰ sweptback wing of aspect ratio 3 with conical camber and designed for a mach number of 2 (National Aeronautics and Space Administration :, 1961), also by Maarlowe D. Cassetti, Richard J. Re, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Igoe, William B.: Transonic aerodynamic loading characteristics of a wing-body-tail combination having 52.5° sweptback wing of aspect ratio 3 with conical wing camber and body indentation for a design Mach number [square root of] 2 (National Aeronautics and Space Administration, 1961), also by Marlowe D. Cassetti, Richard J. Re, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Igoe, William B.: Wind-tunnel buffeting measurements on two wing end-plate airplane model configurations (National Aeronautics and Space Administration ;, 1967), also by Langley Research Center (page images at HathiTrust)
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