At first, the current status of solid riveting processes is reviewed, and the key influencing factors on static/fatigue failure of riveted joints are identified. This paper aims to present a practical review on current practice and novel techniques of solid riveting for aircraft applications in order to obtain a thorough understanding of the underlying mechanisms of defect development to assist industrial users to find pragmatic solutions for safe life extension of components. * e-mail: riveting is the most widely used joining technique in aircraft assembly, and the current key problems affecting practical application and reliable lifting are concentrated on static strength and fatigue. Hongwei Zhao 1 ,2, Jiangjing Xi 2 ,3, Kailun Zheng 4 *, Zhusheng Shi 3, Jianguo Lin 3, Kamran Nikbin 3, Shihui Duan 2 and Binwen Wang 2ĭepartment of Mechanical Engineering, Xi'an Jiaotong University, Xi'an 710000, People's Republic of ChinaĪircraft Strength Research Institute of China, Xi'an 710065, People's Republic of Chinaĭepartment of Mechanical Engineering, Imperial College London, London SW7 2AZ, UKĭepartment of Mechanical Engineering, Dalian University of Technology, Dalian
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