4.7 Article

Prediction of net-tension failure of multi-bolt composite joints: A fast approach for laminates with arbitrary layup

Journal

EUROPEAN JOURNAL OF MECHANICS A-SOLIDS
Volume 87, Issue -, Pages -

Publisher

ELSEVIER
DOI: 10.1016/j.euromechsol.2021.104213

Keywords

Multi-bolt composite joint; Net-tension failure strength; Finite fracture mechanics; Fast approach; P-version finite element analysis

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Funding

  1. Laboratory of Precision Manufacturing Technology, China Academy of Engineering Physics [ZM18004]
  2. Aeronautical Science Foundation of China [201909038001]
  3. Natural Science Foundation of Shanghai [20ZR1462600]
  4. Shanghai Aerospace Science and Technology Innovation Foundation [SAST202020]

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A new fast approach based on finite fracture mechanics and finite element methods was developed to predict the net-tension failure strength of multi-bolt composite joints. The method efficiently calculates stress distribution and stress intensity factor, which can address different problems and validate the results through comparison with test data.
In this study, a new fast approach to predict the net-tension failure strength of multi-bolt composite joints was developed based on finite fracture mechanics and p-version parametric finite element methods. In the proposed approach, stress distribution and stress intensity factor are obtained using the principle of superposition, based on which the problem can be divided into open hole tension and hole bearing problems. The stress distribution and stress intensity factor are determined by using p-version parametric finite element models, which is very computational efficient and can address laminates with arbitrary layup. For the validation purpose, the failure strengths of three multi-bolted joints were predicted and compared to the test data from public literatures, and good agreements were obtained. In addition, the effects of typical parameter variations on the net-tension failure strength were presented by performing a series of parametric studies, which would be a reference for engineering design of multi-bolt composite joints.

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