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首页> 外文期刊>Physics Reports: A Review Section of Physics Letters (Section C) >Collision partner selection schemes in DSMC: From microano flows to hypersonic flows
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Collision partner selection schemes in DSMC: From microano flows to hypersonic flows

机译:DSMC中的碰撞伙伴选择方案:从微/纳米流到高超音速流

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The motivation of this review paper is to present a detailed summary of different collision models developed in the framework of the direct simulation Monte Carlo (DSMC) method. The emphasis is put on a newly developed collision model, i.e., the Simplified Bernoulli trial (SBT), which permits efficient low-memory simulation of rarefied gas flows. The paper starts with a brief review of the governing equations of the rarefied gas dynamics including Boltzmann and Kac master equations and reiterates that the linear Kac equation reduces to a non-linear Boltzmann equation under the assumption of molecular chaos. An introduction to the DSMC method is provided, and principles of collision algorithms in the DSMC are discussed. A distinction is made between those collision models that are based on classical kinetic theory (time counter, no time counter (NTC), and nearest neighbor (NN)) and the other class that could be derived mathematically from the Kac master equation (pseudo-Poisson process, ballot box, majorant frequency, null collision, Bernoulli trials scheme and its variants). To provide a deeper insight, the derivation of both collision models, either from the principles of the kinetic theory or the Kac master equation, is provided with sufficient details. Some discussions on the importance of subcells in the DSMC collision procedure are also provided and different types of subcells are presented. The paper then focuses on the simplified version of the Bernoulli trials algorithm (SBT) and presents a detailed summary of validation of the SBT family collision schemes (SBT on transient adaptive subcells: SBT-TAS, and intelligent SBT: ISBT) in a broad spectrum of rarefied gas-flow test cases, ranging from low speed, internal micro and nano flows to external hypersonic flow, emphasizing first the accuracy of these new collision models and second, demonstrating that the SBT family scheme, if compared to other conventional and recent collision models, requires smaller number of particles per cell to obtain sufficiently accurate solutions. (C) 2016 Elsevier B.V. All rights reserved.
机译:本文的目的是介绍在直接模拟蒙特卡洛(DSMC)方法框架内开发的各种碰撞模型的详细摘要。重点放在新开发的碰撞模型上,即简化的伯努利试验(SBT),该模型允许对稀薄气体流进行有效的低内存模拟。本文首先简要回顾了稀有气体动力学的控制方程,包括玻尔兹曼方程和Kac主方程,并重申了在分子混沌假设下,线性Kac方程可简化为非线性Boltzmann方程。介绍了DSMC方法,并讨论了DSMC中的冲突算法原理。那些基于经典动力学理论的碰撞模型(时间计数器,无时间计数器(NTC)和最近邻居(NN))与其他可以从Kac主方程中数学得出的类别(伪泊松过程,投票箱,主要频率,零碰撞,伯努利试验方案及其变体)。为了提供更深入的见解,从动力学理论或Kac主方程的原理推导了两个碰撞模型,并提供了足够的详细信息。还提供了有关DSMC碰撞过程中子电池重要性的一些讨论,并介绍了不同类型的子电池。然后,本文着重介绍伯努利试验算法(SBT)的简化版本,并详细介绍了SBT系列碰撞方案(瞬态自适应子电池上的SBT:SBT-TAS和智能SBT:ISBT)的验证摘要。从低速,内部微纳流到外部高超音速流的稀有气流测试用例,首先强调了这些新碰撞模型的准确性,其次强调了SBT系列方案(如果与其他常规碰撞和近期碰撞相比)在模型中,每个单元需要较少数量的粒子才能获得足够准确的解。 (C)2016 Elsevier B.V.保留所有权利。

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