Failure analysis of multiple delaminated composite plates due to bending and impact

Bulletin of materials science

S K Bhattacharyya²  P K Sinha¹  P K Parhi¹ 

[1] Department of Aerospace Engineering, Indian Institute of Technology, Kharagpur 721 302, India$$Department of Aerospace Engineering, Indian Institute of Technology, Kharagpur 721 302, IndiaDepartment of Aerospace Engineering, Indian Institute of Technology, Kharagpur 721 302, India$$;Department of Civil Engineering, Indian Institute of Technology, Kharagpur 721 302, India$$Department of Civil Engineering, Indian Institute of Technology, Kharagpur 721 302, IndiaDepartment of Civil Engineering, Indian Institute of Technology, Kharagpur 721 302, India$$

关键词: Failure analysis;    delaminated composite;    bending;    impact.;   

DOI  :  

学科分类：材料工程

来源: Indian Academy of Sciences

【 摘 要 】

The present work aims at the first ply failure analysis of laminated composite plates with arbitrarily located multiple delaminations subjected to transverse static load as well as impact. The theoretical formulation is based on a simple multiple delamination model. Conventional first order shear deformation is assumed using eight-noded isoparametric quadratic elements to develop the finite element analysis procedure. Composite plates are assumed to contain both single and multiple delaminations. For the case of impact, Newmark time integration algorithm is employed for solving the time dependent multiple equations of the plate and the impactor. Tsai-Wu failure criterion is used to check for failure of the laminate for both the cases. To investigate the first ply failure, parametric studies are made for different cases by varying the size and number of delaminations as well as the stacking sequences and boundary conditions.

【 授权许可】

Unknown