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首页> 外文期刊>Physics of fluids >Vortex-accelerated secondary baroclinic vorticity deposition and late-intermediate time dynamics of a two-dimensional Richtmyer-Meshkov interface
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Vortex-accelerated secondary baroclinic vorticity deposition and late-intermediate time dynamics of a two-dimensional Richtmyer-Meshkov interface

机译:二维Richtmyer-Meshkov界面的涡旋加速次级斜压涡旋沉积和中后期时间动力学

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摘要

We study the vortex-accelerated secondary baroclinic vorticity deposition (VAVD) at late-intermediate times, and dynamics of sinusoidal single-mode Richtmyer-Meshkov interfaces in two dimensions. Euler simulations using a piecewise parabolic method are conducted for three post-shock Atwood numbers (A*), 0.2, 0.635, and 0.9, with Mach number (M) of 1.3. We initialize the sinusoidal interface with a slightly "diffuse" or small-but-finite thickness interfacial transition layer to facilitate comparison with experiment and avoid ill-posed phenomena associated with evolutions of an inviscid vortex sheet. The thickness of the interface is chosen so that there are no secondary structures along the interface prior to the multivalue time t(M), which is defined as the time when the extracted medial axis of an interfacial layer first becomes multivalued. For an interval of 11t(M) beyond t(M), the simulations reveal nearly monotonic strong growth of both positive and negative baroclinic circulation in a vortex bilayer pattern inside the complex roll-up region. The circulations grow and secondary baroclinic circulation dominates at intermediate times, especially for higher A*. This vorticity deposition is due to misalignment of density gradient across the interface and vortex-centripetal acceleration (secondary baroclinic), and enhanced by the intensification of interfacial density gradient arising from the vortex-induced strain. Our simulation results for A*=0.635 agree with the recent air-sulfur hexafluoride (SF6) experiment of Jacobs and Krivets [Proceedings of the 23rd International Symposium on Shock Waves, Fort Worth, Texas, (2001)], including several large-scale features of the evolving mushroom structure: The usual interface spike-bubble amplitude growth rate (a)over dot and the dimensions of the spike roll-up cavity. VAVD plays an important role in the intermediate time dynamics of the interfaces. Our amplitude growth rate a disagrees with the O(t(-1)) result of Sadot [Phys. Rev. Lett. 80, 1654 (1998)]. Instead, it approaches a constant which increases with A*(less than or equal to0.9). An adjusting periodic single point vortex model which uses the calculated net circulation magnitude and its location, gives excellent results for the amplitude growth rates to late-intermediate times at low Atwood numbers (A*=0.2,0.635). The evolution of enstrophy, vorticity skewness, and flatness are quantified for the entire run duration, and one-dimensional averaged kinetic-energy spectra are presented at several times. (C) 2003 American Institute of Physics. [References: 38]
机译:我们研究了后期中期的涡旋加速次级斜压涡度沉积(VAVD),以及二维二维正弦单模Richtmyer-Meshkov界面的动力学。对三个震后阿特伍德数(A *),0.2、0.635和0.9(马赫数(M)为1.3)进行了使用分段抛物线法的Euler模拟。我们使用略微的“扩散”或较小但厚度有限的界面过渡层来初始化正弦界面,以便于与实验进行比较,并避免与无粘性涡旋片的演化相关的不适定现象。选择界面的厚度,以便在多值时间t(M)之前沿界面没有二级结构,该时间定义为提取的界面层中轴首先变为多值的时间。对于超出t(M)的11t(M)间隔,模拟显示正负斜压循环几乎呈单调强劲增长,呈复杂卷起区域内的涡旋双层模式。在中间时间,循环增加,次要斜压循环占主导地位,尤其是对于较高的A *。这种涡流沉积是由于界面上密度梯度的不对准和涡心向加速度(二次斜压)引起的,并且由于涡流诱发的应变引起的界面密度梯度的增强而增强。我们对A * = 0.635的模拟结果与Jacobs和Krivets最近的空气六氟化硫(SF6)实验[第23届冲击波国际研讨会论文集,得克萨斯州沃思堡,(2001)]一致,其中包括一些大型的蘑菇结构不断演变的特征:通常的界面尖峰气泡振幅在点上的增长率(a)和尖峰卷起腔的尺寸。 VAVD在界面的中间时间动态中起着重要作用。我们的幅度增长率a与Sadot的O(t(-1))结果不同。牧师80,1654(1998)]。相反,它接近一个随A *(小于或等于0.9)增加的常数。使用计算出的净循环量及其位置的调整周期单点涡旋模型,在低阿特伍德数(A * = 0.2,0.635)时,到后期中期的幅度增长率均获得了极好的结果。在整个运行过程中,对涡旋,涡度偏斜和平坦度的演变进行了量化,并多次展示了一维平均动能谱。 (C)2003美国物理研究所。 [参考:38]

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