Thickness effects on the compressive stiffness and strength of stitched composite laminates

被引:10
|
作者
Gunnion, AJ
Scott, ML
Thomson, RS
Hachenberg, D
机构
[1] Cooperat Res Ctr Adv Composite Struct, Fishermans Bend, Vic 3207, Australia
[2] RMIT Univ, Sir Lawrence Wackett Ctr Aerosp Design Technol, Melbourne, Vic 3001, Australia
[3] Airbus Deutschland GmbH, D-21111 Hamburg, Germany
关键词
D O I
10.1016/j.compstruct.2004.04.071
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A finite element unit cell model for predicting the 3-D mechanical properties of laminates with through-thickness reinforcement has been developed using a unique voxel mesh approach. As part of its development, the model is being verified to other models and validated with experimental data. The model has been validated to tensile experimental data with much success. For further validation of the model and its assumptions, an experimental program was conducted to investigate the compressive properties of stitched laminates for three different thicknesses. It was found that the unstitched modulus remained independent of thickness, while the stitched modulus increased with thickness due to spreading and kinking of the outer surface plies during the stitch formation process. The model predicted the change in modulus well, however did not capture the thickness effect observed in the experimental results. While it was found that stitching did have an influence on the in-plane compressive properties of the test specimens, the known damage tolerance and manufacturing advantages of stitched laminates are considered to outweigh any penalties for certain critical applications. (C) 2004 Elsevier Ltd. All rights reserved.
引用
收藏
页码:479 / 486
页数:8
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