ABSTRACT
Bolted composite joints are one of the most common joining methods used in aerospace industry for joining of parts and sub-assemblies, where there is a need to transfer high load with consistency and easy to assemble/ dissemble of parts for maintenance. Bolted connection undergoes different types of vibrations during their service life, that make the pre-load on bolted joints to decrease and call for increase in dynamic loading and failure. Regular checking and tightening of bolted joints become a crucial and expensive activity to maintain the structure to perform efficiently. The natural frequency is one of the most important factors of vibration of structure that depends on the geometry and material properties of the structure. In this paper, the effect of pre-load and temperature on the natural frequency of single bolted and double-bolted joints is investigated experimentally and numerically.
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Notes on contributors
Salam Abdus
Salam Abdus is a mechanical engineer having more than 10 years of experience blended with diversified skills dealing with maintenance, design and management. Currently he is doing Ph.D. in Flight vehicle design/ composite structure design technology in the university of Beihang, Beijing China.
Xiaoquan Cheng
Xiaoquan Cheng is a Professor in Flight vehicle design/ composite structure design technology. His profile is listed at http://shi.buaa.edu.cn/chengxiaoquan/zh_CN/index.htm
Yujia Cheng
Yujia Chengis a lab assistant having expertise of testing and manipulation of technical data.
Renwei Hu
Renwei Hu is a professor inf Flight vehicle design/ composite structure design technology.
Abid Muhammad
Abid Muhammad is a Ph.D. student. He has experience in mechanical Design and numerical simulation.