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AN EDDY CHARACTERISTIC TIME MODELING IN LES FOR GAS TURBINE COMBUSTOR

机译:燃气轮机燃烧器LES中的涡旋特性时间模型

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For calculating turbulent flame characteristics such as temperature and chemical species in the gas turbine combustor, an effort applying Large Eddy Simulation (LES) to a combustion simulation has been made in recent years. However, there is no established method of estimating reaction rate on LES combustion simulation. In this paper, we construct an eddy characteristic time derived from large-scale motion to calculate the combustion reaction rate using an eddy dissipation concept model (EDC) and estimate combustion characteristics (temperature and chemical species distribution) in the combustor for the purpose of solving fundamental problems of gas turbine combustor such as swirling effect or formation of pollutant products. As a result, it is shown that the combustion simulation using LES with EDC model is effective method to calculate the characteristics of turbulent diffusion flame such as gas turbine combustor.
机译:为了计算燃气轮机燃烧器中温度和化学物质的湍流火焰特性,近年来已经提出了将大涡模拟(LES)应用于燃烧模拟的努力。然而,没有建立估算LES燃烧模拟对反应速率的方法。在本文中,我们构造了源自大规模运动的涡旋特性时间,以计算使用涡流耗散概念模型(EDC)和燃烧器中的燃烧特性(温度和化学物质分布)来计算燃烧特性,以便解决燃气轮机燃烧器的根本问题,如旋流效果或污染物的形成。结果,示出了使用具有EDC模型的LES的燃烧模拟是计算湍流扩散火焰的特性,例如燃气涡轮燃烧器的特性。

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