Browse > Article
http://dx.doi.org/10.5139/IJASS.2017.18.1.63

A Study on a Composite Laminate Pull-through Joint  

Kwon, Jeong-Sik (Department of Aerospace & Mechanical Engineering, Korea Aerospace University)
Kim, Jin-Sung (Department of Aerospace & Mechanical Engineering, Korea Aerospace University)
Seo, Bum-Kyung (Department of Aerospace & Mechanical Engineering, Korea Aerospace University)
Lee, Soo-Yong (Department of Aerospace & Mechanical Engineering, Korea Aerospace University)
Publication Information
International Journal of Aeronautical and Space Sciences / v.18, no.1, 2017 , pp. 63-69 More about this Journal
Abstract
In this paper, composite laminate pull-through resistance was analyzed using the FEM method and compared with test results. 2D and 3D simplified FEM models, a nonlinear analysis, and a progressive failure analysis utilizing three composite laminate failure theories Maximum Stress, Maximum Strain, and Tsai-Wu were used to predict the FEM results with the test results. The load and boundary conditions of the test were applied to the FEM to simulate the test. A composite laminate pull-through test (ASTM D7332 Proc. B) was designed with a special fixture to collect more precise data. The test results were compared with the FEM analysis results.
Keywords
ASTM D7332; Fixture Design; FEM; Nonlinear Analysis; Progressive Failure Analysis (PFA); Composite Failure Theory;
Citations & Related Records
연도 인용수 순위
  • Reference
1 ASTM D 7332, Standard Test Method for Measuring the Fastener Pull-Through Resistance of a Fiber-Reinforced Polymer Matrix Composite.
2 ASM Handbook, Vol. 21, pp. 1796-1811.
3 Cwik, T., Iannucci, L. and Effenberger, M., "Pullthrough Performance of Carbon Fiber Epoxy Composites", Composite Structures, Vol. 94, No. 10, 2012, pp. 3037-3042.   DOI
4 Elder, D. J., Verdaasdonk, A. H. and Thomson, R. S., "Fastener Pull-through in a Carbon Fiber Epoxy Composite Joint", Composite Structures, Vol. 86, No. 1, 2008, pp. 291-298.   DOI
5 Banbury, A., Kelly, D. W. and Jain, L. K., "A Study of Fastener Pull-through Failure of Composite Laminates Part 2: Failure Prediction", Composite Structures, Vol. 45, No. 4, 1999, pp. 255-270.   DOI
6 Kelly, G. and Hallstrom, S., "Strength and Failure Mechanisms of Composite Laminates Subject to Localized T ransverse Loading", Composite Structures, Vol. 69, No. 3, 2005. pp. 301-314.   DOI
7 Banbury, A. and Kelly, D. W., "A Study of Fastener Pull-through Failure of Composite Laminates Part 1: Experimental", Composite Structures, Vol. 45, No. 4, 1999, pp. 241-254.   DOI
8 HL12, 13, 523 specifications http://www.lisi-aerospace.com
9 Pearce, G. M. K., Johnson, A. F., Hellier, A. K. and Thomson, R. S., "A Study of Dynamic Pull-through Failure of Composite Bolted Joints Using the S Tacked-shell Finite Element Approach", Composite Structures, Vol. 118, 2014, pp. 86-93.   DOI
10 Catalanotti, G., Camanho, P. P., Ghys, P. and Marques, A. T., "Experimental and Numerical Study of Fastener Pullthrough Failure in GFRP Laminates", Composite Structures, Vol. 94, No. 1, 2011, pp. 239-245.   DOI
11 MSC. Nastran 2014 Nonlinear User's Guide SOL 400.