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Experimental and Numerical Study of Turbulent Mixing Behind a Model Turbomeca Swirl Burner

机译:模型涡轮机旋流燃烧器湍流混合的实验与数值研究

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This paper reports on the investigation of flow structure and turbulent mixing in model Turbomeca swirl burner at atmospheric pressure with different Reynolds numbers by optical diagnostics (planar laser-induced fluorescence) and numerical simulation (large eddy simulation). The numerical simulation shows the good agreement with the experimental results. The operating modes of the combustion chamber presented in the work show unsatisfactory mixing of air with fuel in the initial region of the flow. In order to provide good mixing air and fuel at the atmospheric pressure in initial region of the flow after nozzle it is necessary supply fuel into the premixer through small channels.
机译:本文通过光学诊断(平面激光诱导的荧光)和数值模拟(大涡模拟)不同雷诺数在大气压下模型涡轮旋流燃烧器流动结构和湍流混合的研究。 数值模拟显示了与实验结果的良好一致性。 在工作中提出的燃烧室的操作模式显示出在流动初始区域中具有燃料的空气的令人不令人满意的混合。 为了在喷嘴之后提供初始区域的初始区域的大气压下提供良好的混合空气和燃料,这是通过小通道向预混合剂供应燃料。

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