首页> 外文会议>ASME Turbo Expo: Turbomachinery Technical Conference and Exposition >LARGE EDDY SIMULATION OF A TURBULENT SPRAY BURNER USING THICKENED FLAME MODEL AND ADAPTIVE MESH REFINEMENT
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LARGE EDDY SIMULATION OF A TURBULENT SPRAY BURNER USING THICKENED FLAME MODEL AND ADAPTIVE MESH REFINEMENT

机译:使用加厚火焰模型和自适应网格改进的湍流喷涂机的大涡模拟

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The accurate simulation of two-phase flow combustion is crucial for the design of aeronautical combustion chambers. In order to gain insight into complex interactions between a flame, a flow, and a liquid phase, the present work addresses the combustion modeling for the Large Eddy Simulation (LES) of a turbulent spray jet flame. The Eulerian-Lagrangian framework is selected to represent the gaseous and liquid phases, respectively. Chemical processes are described by a reduced mechanism, and turbulent combustion is modeled by the Thickened Flame Model (TFM) coupled to the Adaptive Mesh Refinement (AMR). The TFM-AMR extension on the dispersed phase is successfully validated on a laminar spray flame configuration. Then, the modeling approach is evaluated on the academic turbulent spray burner, providing a good agreement with the experimental data.
机译:两相流燃烧的精确模拟对于航空燃烧室的设计至关重要。为了深入了解火焰,流动和液相之间的复杂相互作用,本作者解决了湍流喷射喷射火焰的大涡模拟(LES)的燃烧建模。选择欧拉拉拉格兰师框架分别代表气态和液相。通过减少机构描述了化学过程,并且通过耦合到自适应网格细化(AMR)的增稠火焰模型(TFM)来建模湍流燃烧。分散相的TFM-AMR延伸在层流式喷雾火焰配置上成功验证。然后,在学术湍流喷雾器上评估建模方法,提供与实验数据的良好一致性。

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