A study of transverse normal stress effect on vibration of multilayered plates and shells

被引:184
作者
Carrera, E [1 ]
机构
[1] Politecn Torino, Dept Aeronaut & Aerosp Engn, I-10129 Turin, Italy
关键词
D O I
10.1006/jsvi.1999.2271
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
This paper evaluates transverse normal stress sigma(zz) effect on vibration of multilayered structures. To this purpose a mixed plate model initially introduced by Toledano and Murakami has been extended to dynamics analysis of double curved shells. These models allow both continuous interlaminar transverse shear and normal stresses as well as the zigzag form of the displacement distribution in the shell thickness directions to be modelled. Governing equations have been derived by employing a Reissner's mixed theorem. Classical models on the basis of standard displacement formulations have been considered for comparison purposes. The evaluations of transverse stress effects have been conducted by comparing constant, linear and higher order distributions of transverse displacement components in the plate thickness directions. Free vibrational response of layered, simply supported plates, cylindrical and spherical shells made of isotropic as well as orthotropic layers has been analyzed. The numerical investigation carried out and comparison with earlier results has concluded that: 1. The possibility of describing a priori interlaminar continuous transverse normal stress sigma(zz) makes the mixed theories more attractive with respect to other available modelling. 2. Any refinements of classical models are meaningless, unless the effects of interlaminar continuous transverse shear and normal stresses are both taken into account in a multilayered shell theory. (C) 1999 Academic Press.
引用
收藏
页码:803 / 829
页数:27
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