325 Approximate Analysis of Laminated Composite Curved Panel Using Higher-Order Shear Deformation Theory

2002 ◽  
Vol 2002.15 (0) ◽  
pp. 265-266
Author(s):  
Jianwei SHI ◽  
Akihiro NAKATANI ◽  
Hiroshi KITAGAWA
2004 ◽  
Vol 20 (3) ◽  
pp. 238-246
Author(s):  
Shi Jianwei ◽  
Nakatani Akihiro ◽  
Kitagawa Hiroshi

1984 ◽  
Vol 51 (4) ◽  
pp. 745-752 ◽  
Author(s):  
J. N. Reddy

A higher-order shear deformation theory of laminated composite plates is developed. The theory contains the same dependent unknowns as in the first-order shear deformation theory of Whitney and Pagano [6], but accounts for parabolic distribution of the transverse shear strains through the thickness of the plate. Exact closed-form solutions of symmetric cross-ply laminates are obtained and the results are compared with three-dimensional elasticity solutions and first-order shear deformation theory solutions. The present theory predicts the deflections and stresses more accurately when compared to the first-order theory.


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