The Online Books Page

Books by Robert W. Dunning:

Books in the extended shelves:

• Dunning, Robert W.: Aerodynamic characteristics of two delta wings and two trapezoidal wings at Mach number of 4.04 (National Advisory Committee for Aeronautics, 1959), also by Fred M. Smith, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Dunning, Robert W.: Factors affecting the maximum lift-drag ratio at high supersonic speeds (National Advisory Committee for Aeronautics, 1956), also by Charles H. McLellan, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Dunning, Robert W.: Normal force, center of pressure, and zero-lift drag of several ballistic-type missiles at Mach numbers of 4.05 (National Advisory Committee for Aeronautics, 1954), also by Edward F. Ulmann, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Dunning, Robert W.: Some effects of fin plan form on the static stability of fin-body combinations at Mach number 4.06 (National Advisory Committee for Aeronautics, 1952), also by Edward F. Ulmann, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Dunning, Robert W.: The static stability characteristics of several preliminary models of the X-15 research airplane at Mach numbers of 2.98 and 4.01 (National Aeronautics and Space Administration, 1959), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)

Find more by Robert W. Dunning at your library, or elsewhere.