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发表时间:2022-10-10
发表刊物:宇航学报
卷号:24
期号:1
页面范围:88-91
ISSN号:1000-1328
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上一条:Robust topology optimization for dynamic compliance minimization under uncertain harmonic excitations with inhomogeneous eigenvalue analysis
下一条:Parametric study of bonded steel-concrete composite beams by using finite element analysis