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THE EFFECTS OF HIGH MAINSTREAM TURBULENCE AND TURBINE VANE FILM COOLING ON THE DISPERSION OF A SIMULATED HOT STREAK

机译:高主流湍流和涡轮叶片冷却对模拟热条纹色散的影响

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This paper presents the combined effects of high turbulence and film cooling on the dispersion of a simulated hot streak as it passes over a scaled-up nozzle guide vane. Experimental data demonstrates a considerable decay in the strength of a hot streak due to turbulence effects alone. Film cooling further reduces the peak temperature values resulting in a reduction of the peak temperature in the hot streak on the order of 75% relative to the upstream peak temperature in the hot streak. Comparisons are made between high turbulence (Tu = 20%) and moderate turbulence (Tu = 3.5%) as well as between different blowing conditions for the suction side, showerhead, and pressure side film cooling holes on a simulated nozzle guide vane.
机译:本文介绍了湍流和薄膜冷却对模拟热条纹在通过按比例放大的喷嘴导流叶片时的分散性的综合影响。实验数据表明,仅由于湍流效应,热条纹的强度就会大大降低。薄膜冷却进一步降低了峰值温度值,导致热条纹中的峰值温度相对于热条纹中的上游峰值温度降低了约75%。比较了高湍流(Tu = 20%)和中湍流(Tu = 3.5%)以及模拟喷嘴导向叶片上的吸入侧,喷头和压力侧薄膜冷却孔的不同吹制条件。

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