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RESEARCH PAPERS

Response of Cylindrical Sandwich Shells to Moving Loads

[+] Author and Article Information
G. Herrmann

The Technological Institute, Northwestern University, Evanston, Ill.

E. H. Baker

Structural Sciences, Space and Information Systems Division, North American Aviation, Inc., Downey, Calif.

J. Appl. Mech 34(1), 81-86 (Mar 01, 1967) (6 pages) doi:10.1115/1.3607672 History: Received November 17, 1965; Revised March 18, 1966; Online September 14, 2011

Abstract

This paper presents an analysis into the dynamic response of a long cylindrical sandwich shell under a moving axially symmetric ring load. The shell is assumed to be orthotropic and subjected to an initial axial stress. The uniform velocity of the load is prescribed and only the steady-state response is considered. Numerical results indicate the effects of various relevant parameters. The behavior of orthotropic sandwich cylinders under initial stress is compared with that of homogeneous isotropic cylindrical shells free of initial stress, and differences are pointed out.

Copyright © 1967 by ASME
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