期刊
ADVANCES IN AIRCRAFT AND SPACECRAFT SCIENCE
卷 1, 期 2, 页码 145-175出版社
TECHNO-PRESS
DOI: 10.12989/aas.2014.1.2.145
关键词
static analysis; arbitrarily shaped plates; stress and strain recovery; generalized differential quadrature; strong formulation finite element method
资金
- Italian Ministry for University and Scientific, Technological Research MIUR
The results of a series of numerical experiments are presented to verify some of the important developments made in the first part of this paper. Firstly, the static solution of an algebraic system obtained through Strong Formulation Finite Element Method (SFEM) is presented. Secondly, the stress and strain recovery procedure is descripted for the present technique. It will be clear that the present approach is suitable for any strong formulation finite element methodology, due to the presented general approach based on the unknown displacements and on the elasticity equations. Thirdly, the numerical solutions for some classical and other numerical results found in literature are exposed. Finally, an arbitrarily shaped composite plate is solved and good agreement is observed for all the presented cases.
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