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首页> 外文期刊>Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow >Unsteady characteristics of the static stall of an airfoil subjected to freestream turbulence level up to 16%
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Unsteady characteristics of the static stall of an airfoil subjected to freestream turbulence level up to 16%

机译:受到高达16%的自由流湍流影响的机翼静态失速的不稳定特性

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摘要

Fluctuation of the separation point on an airfoil under high turbulence level is investigated using pressure measurements and flow visualisations. The characteristics of the unsteady loads induced by Karman vortex shedding are studied. This is related with a local approach based on the study of the oscillation zone. A method based on the pressure standard deviation is proposed to obtain the length of this zone, which is found to be independent of the turbulence level. This result is in agreement with that obtained by spectral analysis which shows no effect of the turbulence level on the Karman vortex shedding frequency.
机译:使用压力测量和流量可视化技术研究了高湍流水平下翼型上分离点的波动。研究了卡曼涡旋脱落引起的非定常载荷的特性。这与基于振动区研究的局部方法有关。提出了一种基于压力标准偏差的方法来获得该区域的长度,该长度与湍流水平无关。该结果与通过光谱分析获得的结果一致,该光谱分析显示湍流水平对Karman涡旋脱落频率没有影响。

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