Dynamic Charateristics of Composite Plates Based On a Higher Order Theory Under Low-Velocity Impact

저속 충격시 고차이론을 이용한 복합재료 판의 동적 특성

  • 심동진 (한국과학기술원 항공우주공학과 대학원) ;
  • 김지환 (한국과학기술원 항공우주공학과)
  • Published : 1997.04.01

Abstract

The dynamic response of symmetric cross-ply and angle-ply composite laminated plates under impact loads is investigated using a higher order shear deformation theory. A modified Hertz law is used to predict the impact loads and a four node finite element is used to model the plate. By using a higher order shear deformation theory, the out-of-plane shear stresses, which can be a crucial factor in the failure of composite plates, are determined with significant accuracy. The results compared with previous investigations showed good agreement. The effect of ply sequence and ply angle on the contact force is also studied.

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