A six-variable geometrical nonlinear shear deformation laminated theory is
presented in which normal stress and strain distribution can be calculated.
By considering some affective factors-that were neglected under the finite
deformation condition, an improved Von Karman geometrical nonlinear deform
ation-strain relation is used for large deformation analysis. By analyzing
the bending problem of laminated plates, and by comparing it with 3-D elast
icity solutions and J.N. Reddy five-variable simple higher-order shear defo
rmation laminated theory, we can come to a,conclusion that a satisfying pre
cision of the calculation studied in this paper has been achieved, which sh
ows that it is especially suitable for application of the calculation in th
e condition of a large deformation and the laminated thick plate analysis.
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