The dynamic buckling problem caused by propagation of stress wave in elastic cylindrical shells under impact torque

1996 ◽  
Vol 17 (1) ◽  
pp. 1-8 ◽  
Author(s):  
Han Qiang ◽  
Ma Hongwei ◽  
Zhang Shanyuan ◽  
Yang Guitong ◽  
Wu Jike
1975 ◽  
Vol 42 (2) ◽  
pp. 316-320 ◽  
Author(s):  
D. Lockhart ◽  
J. C. Amazigo

The dynamic buckling of imperfect finite circular cylindrical shells subjected to suddenly applied and subsequently maintained lateral or hydrostatic pressure is studied using a perturbation method. The geometric imperfections are assumed small but arbitrary. A simple asymptotic expression is obtained for the dynamic buckling load in terms of the amplitude of the Fourier component of the imperfection in the shape of the classical buckling mode. Consequently, for small imperfection, there is a simple relation between the dynamic buckling load under step-loading and the static buckling load. This relation is independent of the shape of the imperfection.


1993 ◽  
Vol 47 (3) ◽  
pp. 399-405 ◽  
Author(s):  
B. Mustafa ◽  
S.T.S. Al-Hassani ◽  
S.R. Reid

1987 ◽  
Vol 23 (6) ◽  
pp. 669-692 ◽  
Author(s):  
H.E. Lindberg ◽  
M.B. Rubin ◽  
L.E. Schwer

1973 ◽  
Vol 40 (3) ◽  
pp. 731-735 ◽  
Author(s):  
S. E. Benzley ◽  
J. R. Hutchinson ◽  
S. W. Key

A theory for thick cylindrical shells is presented that couples the early time thickness stress wave propagation with higher-order shell theory equations. The formulation completely describes the continuum response in the thickness direction for “early time” considerations while representing the circumferential response with a high-order circumferential displacement assumption. Late time (structural response) equations are developed to continue the analysis after thickness effects are no longer important. The finite-element method is used to obtain solutions of the theory. Calculations are presented which show that thickness stress need not be included for cylindrical shells with h/R ratios less than 0.2.


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