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http://dx.doi.org/10.5139/JKSAS.2017.45.1.21

A Study for Failure Test and Progressive Failure Analysis on Composite Laminates Mechanical Joint  

Kwon, Jeong-Sik (Department of Aerospace & Mechanical Engineering, Korea Aerospace University)
Kim, Jin-Sung (Department of Aerospace & Mechanical Engineering, Korea Aerospace University)
Yang, Yong-Man (Department of Aerospace & Mechanical Engineering, Korea Aerospace University)
Lee, Soo-Yong (Department of Aerospace & Mechanical Engineering, Korea Aerospace University)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.45, no.1, 2017 , pp. 21-29 More about this Journal
Abstract
In this paper, the total procedure for composite laminate mechanical joint (ASTM D5961 Proc. A, B) from fixture design to test analysis was showed. Composite laminate mechanical joints were analyzed using the FEM(Finite Element Method) and compared to test results. A progressive failure analysis was applied to FEM to analyze the failure behavior of test specimens. Three failure theories - maximum stress, maximum strain, and Tsai-Wu were applied to FEM to predict test failure load. General parameters for composite laminate joints were reviewed and the differences of bearing strength were compared with major parameters.
Keywords
ASTM D5961; Mechanical Joint; Fixture Design; FEM; Nonlinear Analysis; Progressive Failure Analysis; Composite Failure Theory;
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