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首页> 外文期刊>International Journal for Numerical Methods in Fluids >Compressible air flow through a collapsing liquid cavity
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Compressible air flow through a collapsing liquid cavity

机译:可压缩空气流经坍塌的液体腔

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We present a multiscale approach to simulate the impact of a solid object on a liquid surface: upon impact a thin liquid sheet is thrown upwards all around the rim of the impactor while in its wake a large surface cavity forms. Under the influence of hydrostatic pressure the cavity immediately starts to collapse and eventually closes in a single point from which a thin, needle-like jet is ejected. The existing numerical treatments of liquid impact either consider the surrounding air as an incompressible fluid or neglect air effects altogether. In contrast, our approach couples a boundary-integral method for the liquid with a Roe scheme for the gas domain and is thus able to handle the fully compressible gas stream that is pushed out of the collapsing impact cavity. Taking into account that air compressibility is crucial, since, as we show in this work, the impact crater collapses so violently that the air flow through the cavity neck attains supersonic velocities already at cavity diameters larger than 1 mm. Our computational results are validated through corresponding experimental data.
机译:我们提出了一种多尺度方法来模拟固体对象在液体表面上的撞击:在撞击时,薄薄的液体片会在撞击器的边缘周围向上抛掷,而随后会形成大的表面空腔。在静水压力的作用下,型腔立即开始坍塌,并最终在一个点封闭,从该点喷射出细的针状射流。现有的液体冲击数值处理要么将周围的空气视为不可压缩的流体,要么完全忽略了空气效应。相比之下,我们的方法将液体的边界积分方法与针对气域的Roe方案相结合,因此能够处理从塌陷的撞击腔中推出的完全可压缩的气流。考虑到空气的可压缩性至关重要,因为正如我们在这项工作中显示的那样,撞击坑会剧烈坍塌,以致通过腔颈部的气流在腔直径大于1 mm时就已经达到了超音速。我们的计算结果通过相应的实验数据得到了验证。

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