An Experimental Study on the Shear Buckling of a Composite Plate with Bead and Hole

비드와 원공을 갖는 복합재 평판의 전단 좌굴 실험에 관한 연구

  • 임효식 (군사과학대학원 항공우주공학과) ;
  • 김주언 (공군사관학교 항공공학과) ;
  • 황정선 (공군사관학교 기계공학과)
  • Published : 2000.07.01

Abstract

Buckling behavior was studied for the square plate with bead and hole under shear load. Plates were made to examine the effect of bead and hole to the material, aluminum and composite, the effect of flange angle, bead height and bead radius of curvature. There was little difference between buckling loads obtained by the experiment and Rayleigh-Ritz method to the plate. Buckling load could be increased highly when stress concentration to the hole was dispersed effectively using flange. A well-designed plate using bead and flange showed 3 times as much as stiffness to the plate without bead and flange.

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