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Large eddy simulation of a shocked gas cylinder instability induced turbulence

Science china(physics,Mechanics & Astronomy) 2010年第9期53卷 262-268页

作者： li ping,bai jingsong,wang tao & zou liyong national key laboratory for shock wave and detonation physics research,institute of fluid physics,caep,mianyang 621900,china national key laboratory for shock wave and detonation physics research Institute of Fluid Physics CAEP Mianyang China

The Navier-Stokes equations for compressible fluid are solved with the operator splitting technique and LES (large eddy simulation) with the Smagorinsky model. A computational code MVFT (multi-viscosity-fluid and turbulence) is developed to study hydrodynamic instability and the induced turbulent mixing for multi compressible fluid. In order to validate the code MVFT,the LANL's shock tube experiment of shocked SF6 gas cylinder is simulated with the initial state of SF6 gas cylinder described by dissipative ITL (interface transition layer). It is shown that the width and height of gas cylinder calculated with MVFT are closer to the experimental results than RAGE,and that the velocities of upstream edge,downstream edge and vortex edge agree with the experimental results,and are appreciably smaller than the RAGE results. The code MVFT has been pre-liminarily validated.

关键词： Richtmyer-Meshkov instability large eddy simulation Navier-Stokes equations turbulence model

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Numerical simulation of the hydrodynamic instability experiments and flow mixing

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Science china(physics,Mechanics & Astronomy) 2009年第12期52卷 2027-2040页

作者： bai jingsong wang tao li ping zou liyong liU Cangli national key laboratory for shock wave and detonation physics research Institute of Fluid PhysicsCAEPMianyang 621900China

Based on the numerical methods of volume of fluid (VOF) and piecewise parabolic method (PPM) and parallel circumstance of Message Passing Interface (MPI),a parallel multi-viscosity-fluid hydrodynamic code MVPPM (Multi-Viscosity-fluid Piecewise Parabolic Method) is developed and performed to study the hydrodynamic instability and flow mixing. Firstly,the MVPPM code is verified and validated by simulating three instability cases:The first one is a Riemann problem of viscous flow on the shock tube; the second one is the hydrodynamic instability and mixing of gaseous flows under re-shocks; the third one is a half height experiment of interfacial instability,which is conducted on the AWE's shock tube. By comparing the numerical results with experimental data,good agreement is achieved. Then the MVPPM code is applied to simulate the two cases of the interfacial instabilities of jelly models acceler-ated by explosion products of a gaseous explosive mixture (GEM),which are adopted in our experi-ments. The first is implosive dynamic interfacial instability of cylindrical symmetry and mixing. The evolving process of inner and outer interfaces,and the late distribution of mixing mass caused by Rayleigh-Taylor (RT) instability in the center of different radius are given. The second is jelly layer ex-periment which is initialized with one periodic perturbation with different amplitude and wave length. It reveals the complex processes of evolution of interface,and presents the displacement of front face of jelly layer,bubble head and top of spike relative to initial equilibrium position vs. time. The numerical results are in excellent agreement with that experimental images,and show that the amplitude of initial perturbations affects the evolvement of fluid mixing zone (FMZ) growth rate extremely,especially at late times.

关键词： interfacial instability flow mixing multi-fluid hydrodynamic fluid mixing zone

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激波管实验和果冻实验界面不稳定性数值计算

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应用力学学报 2009年第3期26卷 418-425页

作者：柏劲松王涛邹立勇黄文斌李平中国工程物理研究院流体物理研究所绵阳621900

运用算子分裂技术,增加二阶空间中心差方法和两步Rung-Kutta时间推进方法计算动力学粘性以及热流部分对流场的影响,将可压缩多介质流体动力学高精度欧拉计算方法MFPPM发展到适用于NS(Navier Stokes)方程的可压缩多介质粘性流体计算方法M... 详细信息

运用算子分裂技术,增加二阶空间中心差方法和两步Rung-Kutta时间推进方法计算动力学粘性以及热流部分对流场的影响,将可压缩多介质流体动力学高精度欧拉计算方法MFPPM发展到适用于NS(Navier Stokes)方程的可压缩多介质粘性流体计算方法MVPPM。通过与界面不稳定性实验结果的比较,来检验计算方法的正确性,并验证计算程序的有效性。主要包括一个激波管实验和两个果冻实验,即英国AWE(Atomic Weapons Establishment)激波管实验和LLNL实验室的果冻环实验以及中国工程物理研究院流体物理研究所冲击波物理与爆轰物理实验室进行的爆轰驱动下单层果冻界面不稳定性实验。研究结果表明:数值模拟结果与实验测量结果以及对应时刻的实验图象均吻合较好。

关键词：界面不稳定性激波管高精度计算格式 Navier Stokes方程多介质粘性流体计算方法

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