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Experimental and Numerical Investigation of the Mixing Ratio for Various Vane Swirlers of the Combustion Chamber of a Gas Turbine Engine
Russian Aeronautics Pub Date : 2021-03-12 , DOI: 10.3103/s1068799820040145
T. D. Nguen , Yu. B. Aleksandrov , A. I. Sulaiman , B. G. Mingazov

Abstract

The paper investigates the swirling flow behind the GTE combustion chamber swirler with blades installed under different angles. The mixing ratio in the flow is experimentally analyzed and compared with the estimated values obtained by a numerical approach and using various models of turbulent viscosity.



中文翻译:

燃气轮机燃烧室各种叶片旋流器混合比的实验与数值研究。

摘要

本文研究了以不同角度安装叶片的GTE燃烧室旋流器后面的旋流。对流中的混合比进行实验分析,并将其与通过数值方法和使用各种湍流粘度模型获得的估计值进行比较。

更新日期:2021-03-15
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