On the evaluation of a critical distance approach for failure load prediction of adhesively bonded dissimilar materials

被引:11
作者
Cruz-G, C. E. [1 ]
Akhavan-Safar, A. [2 ]
da Silva, L. F. M. [3 ]
Ayatollahi, M. R. [4 ]
机构
[1] Ctr Ingn & Desarrollo Ind Sede Estado Mexico, Av Desarrollo S-N,Parque Ind Cuamatla, Cuautitlan 54763, Mexico
[2] Inst Sci & Innovat Mech & Ind Engn INEGI, Rua Dr Roberto Frias, P-4200465 Porto, Portugal
[3] Univ Porto, Dept Engn Mecan, Fac Engn, Rua Dr Roberto Frias S-N, P-4200465 Porto, Portugal
[4] Iran Univ Sci & Technol, Sch Mech Engn, Fatigue & Fracture Lab, Tehran 1684613114, Iran
关键词
Critical longitudinal strain; Dissimilar adhesive joints; Failure load prediction; CFRP; Single lap joint; TO-ALUMINUM JOINTS; SINGLE-LAP JOINTS; STIFFNESS BEHAVIOR; STRESS-ANALYSIS; STRENGTH; FRACTURE; THICKNESSES;
D O I
10.1007/s00161-020-00871-7
中图分类号
O414.1 [热力学];
学科分类号
摘要
The validity of the critical longitudinal strain method (CLS) was proved for a wide range of adhesives and substrates employed in bonding similar substrates (same substrate thickness and material). However, the recent need of weight reduction yields a challenge of joining dissimilar materials, especially where composite laminates are bonded to metal substrates. Based on this industrial demand, the need of using a simple approach for failure load estimation of dissimilar adhesive joints is increasing. The aim of this work is to extend the CLS approach to be able to predict the failure load of adhesively bonded dissimilar single lap joints (SLJs). To achieve this, dissimilar SLJs with a brittle adhesive were manufactured and tested. On the other hand, experimental results of other researchers were also considered where composite substrates were bonded to metal adherends. Based on the results, it was found that by doing a minor modification, the already developed CLS method can be successfully applied to dissimilar SLJs. It is shown that the modified CLS method is able to predict the failure load of dissimilar SLJs with both brittle and ductile adhesives.
引用
收藏
页码:1647 / 1657
页数:11
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