Nonlinear Problems in the Dynamics of Thin Shells††These results were obtained in the course of research sponsored partially by the U.S. Army Research Office, Durham, under Grant No. DA-ARO(D)-31-124-G372 with the University of Florida, and partially by the Air Force Flight Dynamics Laboratory, Wright-Patterson Air Force Base, under Contract No. AF33 (657)-10220 with the General Electric Company.
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