这对于高超声速飞行器中液固耦合问题的研究具有一定的实际意义。
The research of hypersonic vehicle for liquid-solid coupling problems has some practical significance.
利用二者模型的底层接口,搭建了液固耦合的轴向柱塞泵虚拟样机模型。
Solid-liquid coupling virtual prototype of axial piston pump was put up based on the interface of the two models.
分析了液固耦合情况下的超声波传播特性,取得了与光弹法物理试验相一致的结果。
Numerical results of the ultrasonic propagation characteristics in a liquid-solid coupled interface are in accord with those obtained by photo-elastic experiments.
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