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IMPLEMENTATION OF DETAILED CHEMISTRY MECHANISMS IN ENGINE SIMULATIONS

机译:在引擎模拟中实现详细的化学机理

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The stiffness of large chemistry mechanisms has been proved to be a major hurdle towards predictive engine simulations. As a result, detailed chemistry mechanisms with a few thousand species need to be reduced based on target conditions so that they can be accommodated within the available computational resources. The computational cost of simulations typically increase super-linearly with the number of species and reactions. This work aims to bring detailed chemistry mechanisms within the realm of engine simulations by coupling the framework of unsteady flamelets and fast chemistry solvers. A previously developed Tabulated Flamelet Model (TFM) framework for non-premixed combustion was used in this study. The flamelet solver consists of the traditional operator-splitting scheme with VODE (Variable coefficient ODE solver) and a numerical Jacobian for solving the chemistry. In order to use detailed mechanisms with thousands of species, a new framework with the LSODES (Livermore Solver for ODEs in Sparse form) chemistry solver and an analytical Jacobian was implemented in this work. Results from 1D simulations show that with the new framework, the computational cost is linearly proportional to the number of species in a given chemistry mechanism. As a result, the new framework is 2-3 orders of magnitude faster than the conventional VODE solver for large chemistry mechanisms. This new framework was used to generate unsteady flamelet libraries for n-dodecane using a detailed chemistry mechanism with 2,755 species and 11,173 reactions. The Engine Combustion Network (ECN) Spray A experiments which consist of an igniting n-dodecane spray in turbulent, high-pressure engine conditions are simulated using large eddy simulations (LES) coupled with detailed mechanisms. A grid with 0.06 mm minimum cell size and 22 million peak cell count was implemented. The framework is validated across a range of ambient temperatures against ignition delay and liftoff lengths. Qualitative results from the simulations were compared against experimental OH and CH_2O PLIF data. The models are able to capture the spatial and temporal trends in species compared to those observed in the experiments. Quantitative and qualitative comparisons between the predictions of the reduced and detailed mechanisms are presented in detail. The main goal of this study is to demonstrate that detailed reaction mechanisms (~1000 species) can now be used in engine simulations with a linear increase in computation cost with number of species during the tabulation process and a small increase in the 3D simulation cost.
机译:大型化学机制的刚度已被证明是预测性发动机仿真的主要障碍。结果,需要根据目标条件减少具有数千种物种的详细化学机制,以便可以将其容纳在可用的计算资源内。模拟的计算成本通常会随着种类和反应数量的增加而线性增加。这项工作旨在通过将非稳定小火焰和快速化学求解器的框架相结合,将详细的化学机理带入发动机仿真领域。在这项研究中使用了以前开发的用于非预混燃烧的表格火焰小火焰模型(TFM)框架。小火焰求解器由具有VODE(变量系数ODE求解器)的传统算子分解方案和用于求解化学反应的数值Jacobian组成。为了使用具有数千个物种的详细机制,这项工作中采用了LSODES(稀疏形式ODE的利弗莫尔求解器)化学求解器和雅可比分析的新框架。一维模拟的结果表明,在新的框架下,计算成本与给定化学机理中物种的数量成线性比例。结果,新的框架比用于大型化学机理的常规VODE求解器快2-3个数量级。使用详细的化学机理,使用了2755种物质和11173个反应,使用这个新框架生成了正十二烷的不稳定小火焰库。发动机燃烧网络(ECN)喷雾使用大型涡流模拟(LES)并结合详细的机理,对由湍流,高压发动机条件下的正十二烷点燃型喷雾组成的实验进行了模拟。实现了具有0.06 mm最小像元大小和2200万个峰值像元数的网格。该框架已在一系列环境温度下针对点火延迟和升起长度进行了验证。将模拟的定性结果与实验OH和CH_2O PLIF数据进行比较。与在实验中观察到的相比,该模型能够捕获物种的时空趋势。减少和详细机制的预测之间的定量和定性比较详细介绍。这项研究的主要目的是证明详细的反应机理(〜1000种)现在可以用于发动机仿真中,并且在制表过程中计算成本随种类的增加而线性增加,而3D仿真成本则有少量增加。

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