Applied Mathematics and Mechanics (English Edition) ›› 1997, Vol. 18 ›› Issue (12): 1137-1152.

• 论文 • 上一篇    下一篇

KÁRMÁN-TYPE EQUATIONS FOR A HIGHER-ORDER SHEAR DEFORMATION PLATE THEORY AND ITS USE IN THE THERMAL POSTBUCKLING ANALYSIS

沈惠申   

  1. Department of Civil Engineering, Shanghai Jiaotong University Shanghai 200030, P. R. China
  • 收稿日期:1996-03-01 修回日期:1997-06-06 出版日期:1997-12-18 发布日期:1997-12-18

KÁRMÁN-TYPE EQUATIONS FOR A HIGHER-ORDER SHEAR DEFORMATION PLATE THEORY AND ITS USE IN THE THERMAL POSTBUCKLING ANALYSIS

Shen Huishen   

  1. Department of Civil Engineering, Shanghai Jiaotong University Shanghai 200030, P. R. China
  • Received:1996-03-01 Revised:1997-06-06 Online:1997-12-18 Published:1997-12-18

摘要:

Kármán-type nonlinear large deflection equations are derived occnrding to the Reddy’s higher-order shear deformation plate theory and used in the thermal postbuckling analysis The effects of initial geometric imperfections of the plate areincluded in the present study which also includes th thermal effects.Simply supported,symmetric cross-ply laminated plates subjected to uniform or nomuniform parabolictemperature distribution are considered. The analysis uses a mixed GalerkinGolerkinperlurbation technique to determine thermal buckling louds and postbucklingequilibrium paths.The effects played by transverse shear deformation plate aspeclraio, total number of plies thermal load ratio and initial geometric imperfections arealso studied.

关键词: higher-order shear deformation plate theory, thermal postbuckling, Galerkin-perturbation technique, composite laminated plate

Abstract:

Kármán-type nonlinear large deflection equations are derived occnrding to the Reddy’s higher-order shear deformation plate theory and used in the thermal postbuckling analysis The effects of initial geometric imperfections of the plate areincluded in the present study which also includes th thermal effects.Simply supported,symmetric cross-ply laminated plates subjected to uniform or nomuniform parabolictemperature distribution are considered. The analysis uses a mixed GalerkinGolerkinperlurbation technique to determine thermal buckling louds and postbucklingequilibrium paths.The effects played by transverse shear deformation plate aspeclraio, total number of plies thermal load ratio and initial geometric imperfections arealso studied.

Key words: composite laminated plate, thermal postbuckling, Galerkin-perturbation technique, higher-order shear deformation plate theory

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