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Math. Comput. Appl. 1996, 1(1), 85-96; doi:10.3390/mca1010085

Dynamic Response of Composite Cylindrical Shells to Shock Loading

Aeronautics and Astronautics Faculty, Istanbul Technical University, Maslak, Istanbul 80626, Turkey
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Published: 1 June 1996
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Abstract

In this paper, dynamic response of composite cylindrical shells subjected to shock loading is studied analytically. The equations of motion are based on Sanders theory of thin shell. The effects of transverse shear deformation and rotatory inertia are taken into account. The circular cylindrical thin shell with simply supported ends is subjected to a shock load, represented by an axially symmetric moving load at a constant speed along the longitudinal direction. The governing equations are solved analytically using the Assumed-Modes Method. The influences of geometrical parameters and composite material properties of circular cylindrical shells on the dynamic response are studied.
This is an open access article distributed under the Creative Commons Attribution License (CC BY 3.0).

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MDPI and ACS Style

Soykasap, Ö.; Mecitoğlu, Z.; Borat, O. Dynamic Response of Composite Cylindrical Shells to Shock Loading. Math. Comput. Appl. 1996, 1, 85-96.

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Math. Comput. Appl. EISSN 2297-8747 Published by MDPI AG, Basel, Switzerland RSS E-Mail Table of Contents Alert
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