A Study on the Stability of Anisotropic Cylindrical Shells

비등방성 원통형 쉘의 안정성에 관한 연구

  • 박근우 (청석엔지니어링 SOC사업부) ;
  • 임성순 (서울시립대 토목공학과) ;
  • 장석윤 (서울시립대 토목공학과)
  • Received : 2000.01.31
  • Published : 2000.04.27


In this paper, stability analysis is carried out for the out of plane behaviors under compressive loads to the direction of the generator in anisotropic cylindrical shells. It is not easy to obtain the analytic solutions about the stability analysis of anisotropic cylindrical shells consisted of composite materials. For solving this problems, this paper used the finite difference method which is one of the numerical methods. Geometrical property of cylindrical shells transforms the compressive loads into the inplane behaviors. This paper studied the change of stiffness in the direction of the circumferential and stability of shells according to change of fiber angle, curvature, subtended angle and aspect ratio. From result of this study, anisotropic cylindrical shells under compressive loads to the direction of the generator vary greatly with respect to the change of the circumferential stiffness. Therefore, it will be more safe to strengthen the circumferential stiffness of anisotropic cylindrical shells under compressive loads.



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