期刊论文详细信息
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES 卷:49
Transient wave analysis of a cantilever Timoshenko beam subjected to impact loading by Laplace transform and normal mode methods
Article
Su, Yu-Chi1  Ma, Chien-Ching1 
[1] Natl Taiwan Univ, Dept Mech Engn, Taipei 10617, Taiwan
关键词: Timoshenko beam;    Bernoulli-Euler beam;    Laplace transform method;    Durbin method;    Normal mode method;    Transient wave;    Resonant frequency;    Slender ratio;   
DOI  :  10.1016/j.ijsolstr.2012.01.013
来源: Elsevier
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【 摘 要 】

This study applies two analytical approaches, Laplace transform and normal mode methods, to investigate the dynamic transient response of a cantilever Timoshenko beam subjected to impact forces. Explicit solutions for the normal mode method and the Laplace transform method are presented. The Durbin method is used to perform the Laplace inverse transformation, and numerical results based on these two approaches are compared. The comparison indicates that the normal mode method is more efficient than the Laplace transform method in the transient response analysis of a cantilever Timoshenko beam, whereas the Laplace transform method is more appropriate than the normal mode method when analyzing the complicated multi-span Timoshenko beam. Furthermore, a three-dimensional finite element cantilever beam model is implemented. The results are compared with the transient responses for displacement, normal stress, shear stress, and the resonant frequencies of a Timoshenko beam and Bernoulli-Euler beam theories. The transient displacement response for a cantilever beam can be appropriately evaluated using the Timoshenko beam theory if the slender ratio is greater than 10 or using the Bernoulli-Euler beam theory if the slender ratio is greater than 100. Moreover, the resonant frequency of a cantilever beam can be accurately determined by the Timoshenko beam theory if the slender ratio is greater than 100 or by the Bernoulli-Euler beam theory if the slender ratio is greater than 400. (C) 2012 Elsevier Ltd. All rights reserved.

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