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RESEARCH PAPERS

Response of Cylindrical Shells to Moving Loads

[+] Author and Article Information
J. P. Jones

Aerospace Corporation, El Segundo, Calif.; University of Southern California, Los Angeles, Calif.

P. G. Bhuta

Space Technology Laboratories, Inc., Redondo Beach, Calif.; University of Southern California

J. Appl. Mech 31(1), 105-111 (Mar 01, 1964) (7 pages) doi:10.1115/1.3629529 History: Received March 13, 1963; Online September 15, 2011

Abstract

The response of a circular cylindrical shell subjected to a moving ring load with a constant velocity has been examined in detail when both longitudinal and transverse coupling effects are included. It is found that the correction in the bending resonance velocity resulting from the inclusion of longitudinal coupling effects is small. The results of the analysis may be used as influence coefficients to determine, by means of Duhamel integrals, the displacements and stresses produced by varying pressure pulses.

Copyright © 1964 by ASME
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