Title of article :
Low-velocity Impact Damage Analysis of Composite Laminates Using Self-adapting Delamination Element Method
Author/Authors :
Lipeng، نويسنده , , Wang and Ying، نويسنده , , Yan and Dafang، نويسنده , , Wu and Hao، نويسنده , , Wu، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2008
Pages :
7
From page :
313
To page :
319
Abstract :
On the basis of a 2D 4-node Mindlin shell element method, a novel self-adapting delamination finite element method is presented, which is developed to model the delamination damage of composite laminates. In the method, the sublaminate elements are generated automatically when the delamination damage occurs or extends. Thus, the complex process and state of delamination damage can be simulated practically with high efficiency for both analysis and modeling. Based on the self-adapting delamination method, linear dy-namic finite element damage analysis is performed to simulate the low-velocity impact damage process of three types of mixed woven composite laminates. Taking the frictional force among sublaminations during delaminating and the transverse normal stress into account, the analytical results are consistent with those of the experimental data.
Keywords :
Delamination , Composite laminate , self-adapting delamination element method , Low-velocity impact
Journal title :
Chinese Journal of Aeronautics
Serial Year :
2008
Journal title :
Chinese Journal of Aeronautics
Record number :
2264731
Link To Document :
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