Buckling Analysis of Laminated Composite Plate and Shell Structures considering a Higher-Order Shear Deformation

고차전단변형을 고려한 복합적층판 및 쉘구조의 좌굴해석

  • 이원홍 (진주산업대학 토목공학과) ;
  • 윤석호 (경동대학교 토목설계과) ;
  • 한성천 (대원전문대학 토목과)
  • Published : 1997.03.30

Abstract

Laminated composite shells exhibit properties comsiderably different from those of the single-layer shell. Thus, to obtain the more accurate solutions to laminated composite shells ptoblems, effects of shear strain should be condidered in analysis of them. A higher-order shear deformation theory requires no shear correction coefficients. This theory is used to determine the buckling loads of elastic shells. The theory accounts for parabolic distribution of the transverse shear through the thickness of the shell and rotary inertia. Exact solutions of simply-supported shells are obtained and the results are compared with the exact solutions of the first-order shear deformation theory, and the classical theory. The present theory predicts the buckling loads more accurately when compared to the first -order and classical theory.

Keywords

References

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