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Flutter of a cylindrical shell subjected to an internal supersonic gas flow
Authors:A. V. Vasil’ev
Affiliation:1.Faculty of Mechanics and Mathematics,Moscow State University,Leninskie Gory, Moscow,Russia
Abstract:The piston theory formula for the excess aerodynamic pressure is used in the majority of works devoted to the flutter of shells. The problem on the flutter of a cylindrical shell subjected to an internal supersonic gas flow is solved in a new formulation
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