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Analytical linear theory for the shock and re-shock of isotropic density inhomogeneities

机译:各向同性密度不均匀性的冲击和再冲击的解析线性理论

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摘要

We present an analytical model that describes the linear interaction of two successive shocks launched into a non-uniform density field. The re-shock problem is important in different fields, inertial confinement fusion among them, where several shocks are needed to compress the non-uniform target. At first, we present a linear theory model that studies the interaction of two successive shocks with a single-mode density perturbation field ahead of the first shock. The second shock is launched after the sonic waves emitted by the first shock wave have vanished. Therefore, in the case considered in this work, the second shock only interacts with the entropic and vortical perturbations left by the first shock front. The velocity, vorticity and density fields are later obtained in the space behind the second shock. With the results of the single-mode theory, the interaction with a full spectrum of random-isotropic density perturbations is considered by decomposing it into Fourier modes. The model describes in detail how the second shock wave modifies the turbulent field generated by the first shock wave. Averages of the downstream quantities (kinetic energy, vorticity, acoustic flux and density) are easily obtained either for two-dimensional or three-dimensional upstream isotropic spectra. The asymptotic limits of very strong shocks are discussed. The study shown here is an extension of previous works, where the interaction of a planar shock wave with random isotropic vorticity/entropy/acoustic spectra were studied independently. It is also a preliminary step towards the understanding of the re-shock of a fully turbulent flow, where all three of the modes, vortical, entropic and acoustic, might be present.
机译:我们提出了一个分析模型,该模型描述了两个连续的冲击向非均匀密度场中的线性相互作用。再冲击问题在不同领域很重要,它们之间是惯性约束融合,在这里需要多次冲击以压缩不均匀的目标。首先,我们提出一个线性理论模型,该模型研究两次连续的冲击与第一次冲击之前的单模密度摄动场的相互作用。在第一次冲击波发出的声波消失后,第二次冲击开始。因此,在这项工作中考虑的情况下,第二次冲击仅与第一次冲击前沿留下的熵和涡旋扰动相互作用。随后在第二次冲击后的空间中获得速度场,涡度场和密度场。根据单模理论的结果,通过将其分解为傅立叶模,可以考虑与全光谱的各向同性密度微扰相互作用。该模型详细描述了第二冲击波如何修改由第一冲击波产生的湍流场。对于二维或三维上游各向同性谱,很容易获得下游量的平均值(动能,涡度,声通量和密度)。讨论了非常强烈的冲击的渐近极限。此处显示的研究是先前工作的扩展,其中独立研究了平面冲击波与各向同性涡度/熵/声谱的相互作用。这也是迈向了解完全湍流重新冲击的第一步,可能同时存在涡流,熵和声波这三种模式。

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