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Stress distribution modeling for interference-fit area of each individual layer around composite laminates joint
Affiliation:1. The Ministry of Education Key Lab of Contemporary Design and Integrated Manufacturing Technology, Northwestern Polytechnical University, Xi''an, 710072, PR China;2. Department of Mechanical and Aerospace Engineering, University of Miami, Coral Gables, FL 33124, United States
Abstract:The discussion about nonuniform stress distribution around interference-fit joint is particular significance in the design of composite laminates structures. In order to investigate the stress distribution of interference-fit area around composite laminates joint, an analytical model is developed for stress distribution based on the Lekhnitskii's complex potential theory. The normal and tangential stresses of contact are achieved by the relationship of deformation between pin and hole. The effects of ply orientation and interference percentage on stress components distributions of each individual layer around symmetrical laminates joint are discussed. In order to verify the validity of the analytical model, extensive 3D finite element models are established to simulate the stress components of laminates interference-fit joint. The results show that the analytical model is valid, and the laminate property and ply orientation have a significant effect on stress distribution trend while interference percentage mainly affects stress magnitude.
Keywords:A  Laminates  B  Residual/internal stress  C  Analytical modeling  E  Joints/joining  Interference fit
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