The Online Books Page

Books by Harry L. Runyan:

Books in the extended shelves:

• Runyan, Harry L.: Appraisal of method of flutter analysis based on chosen modes by comparison with experiment for cases of large mass coupling (National Advisory Committee for Aeronautics, 1949), also by Donald S. Woolston and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Runyan, Harry L.: Compressible, unsteady lifting-surface theory for a helicopter rotor in forward flight (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by H. Tai and Langley Research Center (page images at HathiTrust)
• Runyan, Harry L.: Considerations on the effect of wind-tunnel walls on oscillating air forces for two-dimensional subsonic compressible flow (National Advisory Committee for Aeronautics, 1951), also by Charles E. Watkins and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Runyan, Harry L.: Effect of aerodynamic heating on the flutter of a rectangular wing at a mach number of 2 (National Aeronautics and Space Administration :, 1960), also by Nan H. Jones and Langley Research Center (page images at HathiTrust)
• Runyan, Harry L.: Flutter at very high speeds (National Aeronautics and Space Administration, 1961), also by Homer G. Morgan, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Runyan, Harry L.: Flutter at very high speeds (National Advisory Committee for Aeronautics, 1957), also by Homer G. Morgan, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Runyan, Harry L.: Investigation of flow-field development for a series of sonic-boom wind-tunnel models (National Aeronautics and Space Administration ;, 1971), also by United States National Aeronautics and Space Administration and Langley Research Center (page images at HathiTrust)
• Runyan, Harry L.: Launch-vehicle dynamics (National Aeronautics and Space Administration, 1961), also by A. Gerald Rainey and Langley Research Center (page images at HathiTrust)
• Runyan, Harry L.: NASA TN D-2870 (National Aeronautics and Space Administration :, 1965), also by Harold L. Dodds and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Runyan, Harry L.: On the kernel function of the integral equation relating the lift and downwash distributions of oscillating finite wings in subsonic flow (National Advisory Committee for Aeronautics, 1954), also by Charles E. Watkins, Donald S. Woolston, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Runyan, Harry L.: Single-degree-of-freedom-flutter calculations for a wing in subsonic potential flow and comparison with an experiment (National Advisory Committee for Aeronautics, 1951), also by United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Runyan, Harry L.: Theoretical and experimental investigation of the effect of tunnel walls on the forces on an oscillating airfoil in two-dimensional subsonic compressible flow (National Advisory Committee for Aeronautics, 1955), also by A. Gerald Rainey, Donald S. Woolston, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Runyan, Harry L.: A theoretical and experimental study of wind-tunnel-wall effects on oscillating air forces for two-dimensional subsonic compressible flow (National Advisory Committee for Aeronautics, 1953), also by A. Gerald Rainey, Donald S. Woolston, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)

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