Failure Load Prediction of Composite Joints using Linear Analysis

Author:

Ryu Choong-O1,Choi Jin-Ho2,Kweon Jin-Hwe1

Affiliation:

1. Research Center for Aircraft Parts Technology, School of Mechanical and Aerospace Engineering, Gyeong-Sang National University Jinju, Gyeongnam, 660-701, Korea

2. Research Center for Aircraft Parts Technology, School of Mechanical and Aerospace Engineering, Gyeong-Sang National University Jinju, Gyeongnam, 660-701, Korea,

Abstract

With the wide application of fiber-reinforced composite materials in aero-structures, robotic arms, and mechanical parts, the design of composite joints has become a very important research area. In this article, linear finite element analyses in which the pin of the composite joint is assumed to be a frictionless rigid body are performed and the failure load of the mechanically fastened composite joint is predicted by the failure area index (FAI) method. From these analyses, it has been found that the FAI method can predict the failure loads of composite joints to within 20.1%.

Publisher

SAGE Publications

Subject

Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Reference14 articles.

1. Mallick, P.K. (1988). Fiber-Reinforced Composite, Marcel Dekker, Inc., p. 418.

2. An Experimental Study of the Static Torque Capacity of the Adhesively-Bonded Tubular Single Lap Joint

3. Hart-Smith, L.J. (1980). Mechanically Fastened Joints for Advanced Composites Phenomenological Considerations and Simple Analysis, Fibrous Composite in Structural Design, Plenuum Press, pp. 543—574.

4. Stress Fracture Criteria for Laminated Composites Containing Stress Concentrations

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