Study of numerical analysis and experiment for composite pressure hull on buckling pressure

외압을 받는 복합재 셸의 좌굴해석을 위한 실험 및 수치 해석 연구

  • 정해영 (부산대학교 기계공학부) ;
  • 조종래 (한국해양대학교 기계정보공학부) ;
  • 배원병 (부산대학교 기계공학부) ;
  • 권진회 (경상대학교 기계항공공학부) ;
  • 최진호 (경상대학교 기계항공공학부)
  • Published : 2005.10.01

Abstract

The results of an experimental and analytical study of composite pressure hull on buckling pressure are presented for LRN 300. Composite tensile test was done to know the composite material properties applied FE analysis for URN composite. We predicted the buckling and post buckling analysis of composite laminated cylindrical panels under external compression by using ABAQUS /Standard[Ver 6.4]. To obtain nonlinear static equilibrium solutions for unstable problems, where the load-displacement response can exhibit the type of nonlinear buckling behavior, during periods of the response, the load and/or the displacement may decrease as the solution evolves, used the modified Riks method. The modified Riks method is an algorithm that allows effective solution of such cases [7]. Experiments were conducted to verify the validation of present analysis for cross-ply laminated shells. The shells considered in the study have two different lamination patterns, $[{\pm}45/0/90]_{18s\;and}\;[/0/90]_{18s}$. Cylindrical panel of experiment and analysis have the radius of 200mm, length of 210mm and 60 degree of cutting angle. The critical load from experiment is $69\%$ of that of numerical analysis, because the fracture of matrix was generated before buckling. So URN 300 is not proper to use at the condition under high external pressue.

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