作者: F.-K. Chang , X. L. Qing
DOI: 10.1007/978-94-017-0329-1_4
关键词:
摘要: Joining by mechanical fasteners is one of the common practices in assembly structural components. However, introduce complicated stress field near bolt hole area structures. As a consequence, fastened joints are frequent sources failure aircraft and spacecraft It well known that they can severely reduce load carrying capability components more than fifty percent [1]. Optimal design improves not only integrity performance, but importantly, it considerably minimizes weight structures hence, increase load-carrying capability.