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首页> 外文期刊>High energy density physics >Multicomponent Reynolds-averaged Navier-Stokes simulations of reshocked Richtmyer-Meshkov instability-induced mixing
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Multicomponent Reynolds-averaged Navier-Stokes simulations of reshocked Richtmyer-Meshkov instability-induced mixing

机译:雷奇梅尔-梅什科夫失稳引起的混响的多分量雷诺平均Navier-Stokes模拟

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摘要

A third-order weighted essentially nonoscillatory (WENO) finite-difference implementation of a two-equation K-ε multicomponent Reynolds-averaged Navier-Stokes (RANS) model is used to simulate reshocked Richtmyer-Meshkov turbulent mixing of air and sulfur hexafluoride at incident shock Mach numbers Ma_s = 1.24, 1.50, 1.98 with Atwood number At = 0.67 and Ma_s = 1.45 with At = -0.67. The predicted mixing layer width evolutions are compared with experimental measurements of the width before and after reshock [M. Vetter, B. Sturtevant, Shock Waves 4 (1995) 247; F. Poggi, M.H. Thorembey, G. Rodriguez, Phys. Fluids 10 (1998) 2698] and with the analytical self-similar power-law solution of the simplified model equations before reshock. A new procedure is introduced for the specification of the initial turbulent kinetic energy and its dissipation rate, in which these quantities are related by the linear instability growth rate. The predicted mixing layer widths before reshock are shown to be sensitive to changes in the initial turbulent kinetic energy and its dissipation rate, while the widths after reshock are sensitive to changes in the model coefficients C_(ε0) and σ_ρ appearing in the buoyancy (shock) production terms in the turbulent kinetic energy and dissipation rate equations. A set of model coefficients and initial conditions is shown to predict mixing layer widths in generally good agreement with the pre-reshock experimental data, and very good agreement with the post-reshock data for all cases. Budgets of the turbulent kinetic energy equation just before and after reshock for the Mas = 1.24 case are used to identify the principal physical mechanisms generating turbulence in reshocked Richtmyer-Meshkov instability: buoyancy production (pressure work) and shear production. Numerical convergence of the mixing layer widths under spatial grid refinement is also demonstrated for each of the Mach numbers considered.
机译:两方程K-ε多分量雷诺平均Navier-Stokes(RANS)模型的三阶加权基本非振荡(WENO)有限差分实现用于模拟入射时空气和六氟化硫的湍流混合的Richtmyer-Meshkov湍流混合冲击马赫数Ma_s = 1.24、1.50、1.98,阿特伍德数At = 0.67,Ma_s = 1.45,At = -0.67。将预测的混合层宽度演变与再冲击之前和之后的宽度的实验测量值进行比较[M. Vetter,B.Sturtevant,Shock Waves 4(1995)247; F.波吉(M.H. Thorembey,G。Rodriguez,物理学。流体10(1998)2698],并具有简化的模型方程式在重震前的解析自相似幂律解。为规范初始湍动能及其耗散率引入了一种新程序,其中这些数量与线性不稳定性增长率相关。研究表明,在重新震荡之前的预测混合层宽度对初始湍动能及其耗散率的变化敏感,而在重新震荡之后的宽度对浮力(震荡)中出现的模型系数C_(ε0)和σ_ρ的变化敏感。 )动量动能和耗散率方程中的生产项。示出了一组模型系数和初始条件来预测混合层的宽度,与再冲击前的实验数据基本吻合,并且与所有情况下的再冲击后数据均非常吻合。在Mas = 1.24的情况下,在震后前后的湍动能方程预算用于确定在震后的Richtmyer-Meshkov不稳定性中产生湍流的主要物理机理:浮力产生(压力功)和剪切力产生。对于所考虑的每个马赫数,还证明了在空间网格细化下混合层宽度的数值收敛。

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