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发表时间:2018-01-01
发表刊物:International Journal of Aerospace Engineering
所属单位:运载工程与力学学部
卷号:2018
ISSN号:1687-5966
上一条:Effects of hole-perpendicularity error on joint stiffness of single-lap double-bolt composite joints
下一条:Investigation on temperature field of unidirectional carbon fiber/epoxy composites during drilling process