Composite Iso-Grid Panel Production and Buckling Test

복합재 Iso-Grid 패널 제작 및 좌굴시험

  • 유재석 (한국항공우주연구원 구조그룹) ;
  • 김광수 (한국항공우주연구원 구조그룹) ;
  • 장영순 (한국항공우주연구원 구조그룹)
  • Published : 2004.10.01

Abstract

A composite Iso-grid panel is manufactured and tested by compressive load. Vertical stringers and side stringers are joined with skin by secondary bonding using a liquid type adhesive. Bonding fixtures were developed to attach the stringers to skin. A-scan was done for inspection of secondary bonding region. The out of displacement field is visualized by shadow moire system. The strain and vertical displacement are measured by strain gages and L VDT (Linear Variable Differential Transformer). A local buckling is occurred at all grid sections. After that, the final failure is occurred. The strain of side stringer is much less than that of vertical stringer and skin. Due to the side stringer, the local buckling is delayed. Therefore the ratio of the first buckling to failure load is greater than that of vertical stringer stiffened panel.

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