Analysis of composite stiffener under successive impact and bending test

被引:7
作者
Ridha, Muhammad [1 ]
Tay, Tong-Earn [1 ]
Werner, Sven [2 ]
Joern, Paul [2 ]
Tan, Vincent Beng Chye [1 ]
机构
[1] Natl Univ Singapore, Dept Mech Engn, Singapore, Singapore
[2] Airbus Operat GmbH, Dept ESCRBY Airframe Composite Fuselage R&T, Hamburg, Germany
关键词
Polymer-matrix composites; impact; bending; damage; finite element analysis; LOW-VELOCITY IMPACT; INTERFACE ELEMENTS; EFFICIENT APPROACH; FAILURE ANALYSIS; CAI BEHAVIOR; COMPRESSION; DAMAGE; SIMULATION; STRENGTH; PANELS;
D O I
10.1177/0731684417704076
中图分类号
TB33 [复合材料];
学科分类号
摘要
In this article, we present the analysis, modelling and experimental investigation of composite omega stiffeners from non-penetrating impact to bending-after-impact. We used advanced computational methods to determine the extent of damage due to impact and, without many simplifications to the damage, predict the residual bending-after-impact strength under four-point-bend tests. The predicted sizes and patterns of impact damage, and the subsequent predicted bending strengths are compared to experimental tests of omega stiffeners. This work shows that preserving the details and fidelity of damage in the computational model is critical to successful prediction of residual strength. It was also found that modifying the design of the stiffeners by changing the orientation of some of the plies reduces the extent of impact damage and increases residual bending strength.
引用
收藏
页码:1225 / 1238
页数:14
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