복합재 보강패널의 분리파손 및 좌굴 후 강도 특성

Debonding and Postbuckling Failure Characteristics of Composite Stiffened Panels

  • 김광수 (한국항공우주연구원 구조그룹) ;
  • 유재석 (한국항공우주연구원 구조그룹) ;
  • 안재모 (한국항공우주연구원 구조그룹) ;
  • 장영순 (한국항공우주연구원 구조그룹) ;
  • 이영무 (한국항공우주연구원 우주발사체 기술실)
  • 발행 : 2005.04.29

초록

Compression tests were performed for six types of hat stiffened composite panels with different bonding methods and stiffener section shapes. Six panels showed similar behaviors in buckling and post-buckling region before a skin-stiffener separation failure occurred. The skin-stiffener separation failures occurred in the panels with closed type stiffeners regardless of bonding methods, but not in the panels with open type stiffeners. The separation failures not only reduced the postbuckling strength but also changed buckling mode and postbuckling stiffness. All the separation failures were initiated at the stiffener flange edges closest to skin buckling crests. The co-cured or secondary bonded panels with open type stiffeners had the largest structural performance. Because the post-buckling strength and performance of the composite stiffened panels are reduced by the separation failure, it is important to find bonding methods, stiffener types and manufacturing parameters for preventing of the separation failure.

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