Tensile Test of Composite Laminates and Specimen's Improvement

Article Preview

Abstract:

To obtain the material parameters for the composite laminate structure based on the general strength theory and failure criterion, a series of strength experiments are required to be carried out for some typical laminated fiber reinforced composite laminate plate. Due to complexity of stress state of specimen, some unexpected failure modes will often appear in the tensile test process of composite laminated plate. In this paper, according to the tensile test, the analysis for the failure mechanism of the specimen was executed by using finite element method. The suggestion for suitable geometry of the specimen was put forward, and the experimental results proved that the improvement for the specimen design was effective, thus the success rate of test was improved.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

73-77

Citation:

Online since:

August 2013

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2013 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] S.J. Chen: ACTA AERONAUTICA ET ASTRONAUTICA SINICA, Vol. 29(2008), p.605.

Google Scholar

[2] S.Z. Y. Lin, X.W. Xu and W. Zhu: Journal of Najing University of Aeronautics & Astronautics, Vol. 41 (2009), p.302.

Google Scholar

[3] J. Neogi, J. Sankar and A. D. Kelkar: AIAA Meeting Papers on Disc, (1996), p.515.

Google Scholar

[4] G.Z. Zhu, C.L. Zheng and Y.B. Deng: Science Technology and Engineering, Vol. 11 (2011), p.1527.

Google Scholar

[5] Y.L. Wang, X.Q. Cheng and Z. Fan, et. al.: Acta Materiae Compositae Sinica, Vol. 28 (2011), p.180.

Google Scholar

[6] Y.F. Wu, B.M. Zhang: Fiber Reinforced Plastics/Composites, Vol. 3 (2010), p.29.

Google Scholar

[7] G.T. Zhang, W.G. Chen and B. Yang, et. Al.: FIBER COMPOSITES, Vol. 2 (2009), p.49.

Google Scholar