Dynamic buckling of thin thermoviscoplastic cylindrical shell under radial impulsive loading.pdfVIP
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Dynamic buckling of thin thermoviscoplastic cylindrical shell under radial impulsive loading
ARTICLE IN PRESS
Thin-Walled Structures 44 (2006) 1109–1117
/locate/tws
Dynamic buckling of thin thermoviscoplastic cylindrical shell under
radial impulsive loading
Z.G. Wei, R.C. Batra
Department of Engineering Science and Mechanics, MC 0219, Virginia Polytechnic Institute and State University, Blacksburg, VA 24061, USA
Received 29 March 2006; received in revised form 15 September 2006; accepted 12 October 2006
Available online 1 December 2006
Abstract
The dynamic plastic buckling of a homogeneous and isotropic thin thermoviscoplastic cylindrical shell loaded radially is studied
analytically by analyzing the stability of its stressed/deformed configuration under superimposed infinitesimal perturbations. The wave
number of the perturbation that maximizes its initial growth rate is assumed to determine the buckling mode. Cubic algebraic equations
are obtained for both the maximum initial growth rate of perturbation and the corresponding wave number. The buckled shape of a
cylindrical shell is found to match well with that observed experimentally. The sensitivity of the buckled shape to the impact velocity, the
hardening modulus, and the material viscosity has been delineated. For axially restrained shells, it is found that for materials exhibiting
strain rate hardening only the maximum initial growth rate of the perturbation and the corresponding wave number vary as
ðs0 1=3 2=3 0 1=6 1=3 2=3
¯ =rbÞ h and ðr=s Þ Rb h
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