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Filed under: Subsonic flutter|
- Analytical and experimental study of the effects of wing-body aerodynamic interaction on space shuttle subsonic flutter / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1975), by Richard R. Chipman, Frank J. Rauch, Langley Research Center, and Grumman Aerospace Corporation (page images at HathiTrust)
- Experimental investigation of the effect of aspect ratio and Mach number on the flutter of cantilever wings / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by E. Widmayer, S. A. Clevenston, W. T. Lauten, and Langley Research Center (page images at HathiTrust)
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