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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2001, Vol. 22 ›› Issue (3): 281-283.

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NONLINEAR FINITE ELEMENT METHOD FOR BEAM-SHELL-COMPOSED STRUCTURES

ZHAN Fu-liang, YANG Jia-ling, LI Zai-liang   

  1. Solid Mechanics Research Center, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
  • Received:2000-03-10 Revised:2000-08-31 Online:2001-06-25 Published:2001-06-25

Abstract:

The problems in computing beam-shell-composed structures with the finite element method are pointed out, and a corresponding solution method is proposed based on the finite deformation theory. Numerical examples show the validity and correctness of the present theory. Not only proper for the nonlinear computation of beam-shell-composed structures in large deformation problems, the proposed method is suitable for linear small deformation problems as well.

Key words: beam, plate and shell, composed st ructures, numerical simulatio n, nonlinear finite element, rotation deg ree o f freedom