Tensile Strength Prediction of Out-of-Plane Composite Joints for Integrated Composite Cabins

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Abstract:

The failure of an adhesive-bonded and bolted composite joint under axial tensile loading is investigated. A progressive damage model consisting of a three dimensional FEM accompanying with a three dimensional maximum stress failure criterion and corresponding material degradation model is established to predict the failure behavior of the joint. The predicted failure load and load-displacement curve are validated by the experimental results is obtained. Moreover, the result shows that the discontinuity between two L-shaped laminates is the weak spot and required to be strengthened.

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429-432

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August 2014

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© 2014 Trans Tech Publications Ltd. All Rights Reserved

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