The Online Books Page

Books by Herbert J. Cunningham:

Books in the extended shelves:

• Cunningham, Herbert J.: Analysis of preflutter and postflutter charactristics with motion-matched aerodynamic forces (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Cunningham, Herbert J.: Analytical comparison of effects of solid-friction and viscous structural damping on panel flutter (National Aeronautics and Space Administration ;, 1976), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Cunningham, Herbert J.: Application of a supersonic kernel-function procedure to flutter analysis of thin lifting surfaces (National Aeronautics and Space Administration :, 1970), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Cunningham, Herbert J.: Computer program for supersonic kernel-function flutter analysis of thin lifting surfaces (National Aeronautics and Space Administration ;, 1974), also by Langley Research Center (page images at HathiTrust)
• Cunningham, Herbert J.: Experimental and theoretical studies of panel flutter at Mach number 1.2 to 3.0 (National Advisory Committee for Aeronautics, 1955), also by Maurice A. Sylvester, Herbert C. Nelson, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Cunningham, Herbert J.: Generalization of the subsonic kernel function in the s-Plane, with applications to flutter analysis (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by Robert N. Desmarais and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Cunningham, Herbert J.: NASA TN D-5419 (National Aeronautics and Space Administration ;, 1969), also by Alfredo Navarro Crespo, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Cunningham, Herbert J.: NASA TR R-256 (National Aeronautics and Space Administration ;, 1967), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Cunningham, Herbert J.: Some divergence characteristics of low-aspect-ratio wings at transonic and supersonic speeds (National Aeronautics and Space Administration :, 1960), also by Donald S. Woolston, Frederick W. Gibson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Cunningham, Herbert J.: Steady and unsteady aerodynamic forces from the SOUSSA surface-panel method for a fighter wing with tip missile and comparison with experiment and PANAIR (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Langley Research Center (page images at HathiTrust)
• Cunningham, Herbert J.: A systematic kernel function procedure for determining aerodynamic forces on oscillating or steady finite wings at subsonic speeds (Langley Research Center ;, 1959), also by Charles E. Watkins, Donald S. Wooston, and United States National Aeronautics and Space Administration (page images at HathiTrust)

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