Enhanced modeling of laminated and sandwich plates via strain energy transformation

被引:34
作者
Kim, Jun-Sik
Cho, Maenghyo [1 ]
机构
[1] Seoul Natl Univ, Sch Mech & Aerosp Engn, Seoul 151742, South Korea
[2] Penn State Univ, Dept Aerosp Engn, University Pk, PA 16802 USA
关键词
plate theory; laminate theory; sandwich; shear correction factor;
D O I
10.1016/j.compscitech.2005.11.018
中图分类号
TB33 [复合材料];
学科分类号
摘要
An enhanced first-order shear deformation theory has been developed for the deformation and stress recovery of laminated and sandwich plates. Based on the definition of Reissner-Mindlin's plate theory, the relationships between three-dimensional and first-order shear deformation theories have been derived. It is assumed that the displacements, in-plane strains and stresses of Reissner-Mindlin's plate theory can approximate those of three-dimensional theory, in the least-square sense. Their relationships have been systematically established and verified through the strain energy transformation. These relationships provide the closed-form recovering relations for three-dimensional variables expressed in terms of the variables of Reissner-Mindlin's plate theory. An efficient higher-order plate theory is utilized to obtain the in-plane warping functions. Comparisons of deflection, stresses and shear correction factors of both laminated and sandwich plates using the present theory are made with the original first-order shear deformation theory and three-dimensional exact solutions. (c) 2005 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1575 / 1587
页数:13
相关论文
共 29 条
[1]  
Berdichevsky V.L., 1979, PMM, V43, P664, DOI [10.1016/0021-8928(79)90157-6, DOI 10.1016/0021-8928(79)90157-6]
[2]   Improved mindlin plate stress analysis for laminated composites in finite element method [J].
Cho, M ;
Kim, JS .
AIAA JOURNAL, 1997, 35 (03) :587-590
[3]   A new postprocessing method for laminated composites of general lamination configurations [J].
Cho, M ;
Choi, YJ .
COMPOSITE STRUCTURES, 2001, 54 (04) :397-406
[4]   EFFICIENT HIGHER-ORDER COMPOSITE PLATE-THEORY FOR GENERAL LAMINATION CONFIGURATIONS [J].
CHO, MH ;
PARMERTER, RR .
AIAA JOURNAL, 1993, 31 (07) :1299-1306
[5]   AN EFFICIENT HIGHER-ORDER PLATE-THEORY FOR LAMINATED COMPOSITES [J].
CHO, MH ;
PARMERTER, RR .
COMPOSITE STRUCTURES, 1992, 20 (02) :113-123
[6]   Postprocess method using displacement field of higher order laminated composite plate theory [J].
Cho, MH ;
Kim, JH .
AIAA JOURNAL, 1996, 34 (02) :362-368
[7]  
Dauge M, 1996, ASYMPTOTIC ANAL, V13, P167
[9]   APPLICATION OF THE VARIATIONAL-ASYMPTOTICAL METHOD TO LAMINATED COMPOSITE PLATES [J].
HODGES, DH ;
LEE, BW ;
ATILGAN, AR .
AIAA JOURNAL, 1993, 31 (09) :1674-1683
[10]   RECENT ADVANCES IN ANALYSIS OF LAMINATED BEAMS AND PLATES .1. SHEAR EFFECTS AND BUCKLING [J].
KAPANIA, RK ;
RACITI, S .
AIAA JOURNAL, 1989, 27 (07) :923-934