PDF(1576 KB)
PDF(1576 KB)
PDF(1576 KB)
基于欧拉—拉格朗日方法的复合材料机翼前缘鸟撞模拟
({{custom_author.role_cn}}), {{javascript:window.custom_author_cn_index++;}}Finite Element Analysis of Bird Strike on Composite Wing Leading Edge Based on the Coupling Eulerian-Lagrangian Method
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