|
Flutter of a Cylindrical Shell Subjected to an Internal Supersonic Gas Flow / Vasil'ev A.V. // Vestnik Moskovskogo Universiteta. Seriya 1. Matematika. Mekhanika. 2011. № 5. P. 61-65 [Moscow Univ. Mech. Bulletin. Vol. 66, N 5, 2011.]. 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.
Key words: flutter, cylindrical shell, internal flow.
|