The Online Books Page

Books by Edward C. Polhamus:

Books in the extended shelves:

• Polhamus, Edward C.: Charts for predicting the subsonic vortex-lift characteristics of arrow, delta, and diamond wings (National Aeronautics and Space Administration ;, 1971), also by United States National Aeronautics and Space Administration and Langley Research Center (page images at HathiTrust)
• Polhamus, Edward C.: Drag due to lift at Mach numbers up to 2.0 (National Advisory Committee for Aeronautics, 1953), also by Langley Aeronautical Laboratory and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Polhamus, Edward C.: Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing (National Aeronautics and Space Administration :, 1961), also by Kenneth P. Spreemann and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Polhamus, Edward C.: Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing (National Advisory Committee for Aeronautics, 1958), also by Kenneth P. Spreemann, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Polhamus, Edward C.: NASA TN D-4739 (National Aeronautics and Space Administration ;, 1968), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Polhamus, Edward C.: The rolling moment due to sideslip of swept wings at subsonic and transonic speeds (National Aeronautics and Space Administration, 1960), also by William C. Sleeman (page images at HathiTrust)
• Polhamus, Edward C.: The rolling moment due to sideslip of swept wings at subsonic and transonic speeds (National Advisory Committee for Aeronautics, 1955), also by William C. Sleeman, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Polhamus, Edward C.: A Simple method of estimating the subsonic lift and damping in roll of sweptback wings (National Advisory Committee for Aeronautics, 1949), also by United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Polhamus, Edward C.: Some factors affecting the variation of pitching moment with sideslip of aircraft configurations (Washington, D.C. : National Advisory Committee for Aeronautics, 1955., 1955), also by Langley Aeronautical Laboratory and United States National Advisory Committee for Aeronautics (page images at HathiTrust)

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