首页> 外文会议>2003 ASME(American Society of Mechanical Engineers) Turbo Expo; Jun 16-19, 2003; Atlanta, Georgia >A NEW PARADIGM FOR SIMULATION OF TURBULENT COMBUSTION IN REALISTIC GAS TURBINE COMBUSTORS USING LES
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A NEW PARADIGM FOR SIMULATION OF TURBULENT COMBUSTION IN REALISTIC GAS TURBINE COMBUSTORS USING LES

机译:基于LES的现实燃气轮机湍流燃烧模拟新方法。

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This paper presents a new paradigm for numerical simulation of turbulent combustion in realistic gas turbine combustors. Advanced CFD methods using Large Eddy Simulation (LES) turbulence models are central to this paradigm in fluid dynamics where engineers can apply the full predictive abilities of numerical simulations to the design of realistic gas turbine combustors. The use of LES models is motivated by their demonstrated superiority over RANS to predict turbulent mixing. The subgrid scale models incorporated in LES are based on the dynamic approach where the model coefficients are computed rather than prescribed by the user. This has provided unparalleled robustness to modern turbulent flow computations using LES. A new numerical algorithm was derived that is discretely energy conserving on hybrid unstructured grids, thus allowing numerical simulations at high Reynolds numbers corresponding to operating conditions without using artificial numerical dissipation. This paper deals specifically with the simulation of the gas phase flow through realistic gas turbine combustors and the implementation of combustion and spray models that are needed to predict and control the combustion phenomena in these geometries. Results from several simulations and comparison with experimental data are used to validate this approach. In particular, a complete simulation of the unsteady flow field in a realistic combustor geometry is carried out. Some preliminary results for reacting flow simulations in gas turbine combustors are also discussed. We discuss several challenges related to large-scale simulations of the flow in realistic combustors, including methods to further accelerate the algorithm's convergence (e.g., use of multigrid techniques), improvement of the parallel performance of the flow solver for two-phase flow simulations (e.g., use of dynamic load balancing that accounts for the additional CPU time spent in the spray module when particles are present in the cells).
机译:本文提出了一种用于实际燃气轮机燃烧室湍流燃烧数值模拟的新范例。使用大涡模拟(LES)湍流模型的高级CFD方法是流体动力学这一范式的核心,工程师可以将数值模拟的全部预测能力应用于现实的燃气轮机燃烧器的设计。 LES模型在预测湍流混合方面优于RANS的优越性促使他们使用LES模型。 LES中包含的子网格比例模型基于动态方法,其中模型系数是由用户而不是由用户指定的。这为使用LES的现代湍流计算提供了无与伦比的鲁棒性。推导了一种新的数值算法,该算法在混合非结构化网格上离散地保存能量,因此可以在不使用人工数值耗散的情况下,在与操作条件相对应的高雷诺数下进行数值模拟。本文专门讨论了通过实际燃气轮机燃烧器的气相流模拟以及实现预测和控制这些几何形状中的燃烧现象所需的燃烧和喷雾模型的实现。多次模拟的结果以及与实验数据的比较被用于验证这种方法。特别地,对真实燃烧器几何形状中的非恒定流场进行了完整的模拟。还讨论了一些用于燃气轮机燃烧器中的反应流模拟的初步结果。我们讨论了与现实燃烧器中的大规模流动模拟相关的几个挑战,包括进一步加速算法收敛的方法(例如,使用多网格技术),改进两相流动模拟的流动求解器的并行性能(例如,使用动态负载平衡可解决当单元中存在粒子时在喷涂模块中花费的额外CPU时间)。

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