Buckling Analysis of Laminated Composite Cylindrical Shell under Combined Load State

복합하중상태에 있는 복합재료 원통형 쉘의 좌굴 거동

  • 여경수 (현대건설) ;
  • 양원호 (성균관대학교 기계공학부) ;
  • 조명래 (인덕대학 기계설계과) ;
  • 성기득 (성균관대 기계공학과 대학원)
  • Published : 1999.12.01

Abstract

This paper deals buckling behavior of laminated composite cylindrical shells subjected to combination of axial compression and torison. Linear and nonlinear finite element analysis are carried out . the influence of load type, load ratio, fiber orientation angle, stacking sequence, and intial imperfect on buckling behavior is discussed.

Keywords

References

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