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Compressible air flow through a collapsing liquid cavity

机译:可压缩空气流过塌陷的液体腔

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摘要

We present a multiscale approach to simulate the impact of a solid object ona liquid surface: upon impact a thin liquid sheet is thrown upwards all aroundthe rim of the impactor while in its wake a large surface cavity forms. Underthe influence of hydrostatic pressure the cavity immediately starts to collapseand eventually closes in a single point from which a thin, needle-like jet isejected. Existing numerical treatments of liquid impact either consider thesurrounding air as an incompressible fluid or neglect air effects altogether.In contrast, our approach couples a boundary-integral method for the liquidwith a Roe scheme for the gas domain and is thus able to handle the fully\emph{compressible} gas stream that is pushed out of the collapsing impactcavity. Taking into account air compressibility is crucial, since, as we showin this work, the impact crater collapses so violently that the air flowthrough the cavity neck attains supersonic velocities already at cavitydiameters larger than 1 mm. Our computational results are validated throughcorresponding 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,型腔立即开始塌陷,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的影响。相比之下,我们的方法将液体的边界积分方法与气域的Roe方案相结合,从而能够完全处理从塌陷的撞击腔中推出的气(可压缩)气流。考虑到空气的可压缩性是至关重要的,因为正如我们在这项工作中所示,撞击坑的破裂非常剧烈,以至于流过腔颈的空气在腔直径大于1mm时就已经达到了超音速。通过相应的实验数据验证了我们的计算结果。

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