Research Article
Oct 1968
Forced Motion of Cylindrical Shells
Authors: Herbert Reisman and John MedigeAuthor Affiliations
Publication: Journal of the Engineering Mechanics Division
Volume 94, Issue 5
Abstract
An exact, formal solution is presented for the dynamic response of a circular cylindrical shell of finite length subjected to time-dependent, arbitrarily distributed surface loading. The solution accounts for the effects of shear deformation and rotatory inertia as well as membrane, bending and translational inertia effects. The theory is applied to the case of a freely supported shell subjected to a moving shock, pressure discontinuity. The shock moves with constant speed in a direction which is normal with respect to the shock front, and the angle between the shell axis and the shock front, plane, is arbitrary. The solution so obtained is compared to the corresponding solution within the framework of Flügge shell theory, and significant differences are noted for shells of moderate thickness.
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Published In
Journal of the Engineering Mechanics Division
Volume 94 • Issue 5 • October 1968
Pages: 1167 - 1182
Copyright
© 1968 American Society of Civil Engineers.
History
Published in print: Oct 1968
Published online: Feb 3, 2021
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Herbert Reisman
Prof., Faculty of Engrg. and Applied Sciences, State Univ. of New York, Buffalo, N.Y.
John Medige
Asst. Prof., Faculty of Engrg. and Applied Sciences, State Univ. of New York, Buffalo, N.Y.
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