A QUASI-STATIC PENETRATION MODEL FOR COMPOSITE LAMINATES

被引:48
作者
LEE, SWR
SUN, CT
机构
[1] School of Aeronautics and Astronautics, Purdue University, West Lafayette, IN 47907-1282
关键词
D O I
10.1177/002199839302700302
中图分类号
TB33 [复合材料];
学科分类号
摘要
A quasi-static model was developed to simulate the penetration process of composite laminates. The penetrator was blunt-ended. A series of static punch tests were conducted to characterize the load-displacement relation during penetration. The damage mechanisms were identified by DIB enhanced X-radiography and microscopic observation on sectioned specimens. The major damage modes were found to be delamination and plugging. An axisymmetric finite element analysis was performed to simulate the penetration process. An effective modulus scheme was adopted in the present analysis. Comparison of punch curves showed good agreement between testing and modeling.
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页码:251 / 271
页数:21
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