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Studies on Aero Thermodynamics performance in the Gap between the Base Side and Baseboard of Air Rudders in Arc Wind Tunnel

机译:弧形风洞中空气舵的底侧与底板之间缝隙中空气热力学性能的研究

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The experimental studies on aero thermodynamic performance in the gap between the base side and the baseboard of air rudders were conducted in the arc wind tunnel. The height of the gap was between 3mm and 5mm and the deflection angles of the rudder were respectively 0°,10°and 35°. In the experiments, some parameters such as the cold wall heat fluxes, the static pressures on the baseboard and the rudder post in the gap were measured. The results showed that the cold wall heat fluxes on the baseboard were relatively smaller and first decreased little by little, afterwards, increased to the highest at the rudderpost along the flow when the deflection angle was 0°; On the other hand, the cold wall heat fluxes on the baseboard quickly increased when the deflection angle was more than 0° , especially for those on the rudderpost, and the cold wall heat fluxes and the static pressures on the baseboard became more and more as the deflection increased because of the interaction by the rudder surface and the board. Meanwhile, the ratio of the cold wall heat fluxes on the rudder post and those on the leading edges of the rudder at the same the horizontal position were found with different total enthalpies.
机译:在弧形风洞中进行了空气舵底面与底板之间缝隙内空气热力学性能的实验研究。间隙的高度在3mm至5mm之间,并且舵的偏转角分别为0°,10°和35°。在实验中,测量了一些参数,例如冷壁热通量,底板上的静压力以及间隙中的方向舵柱。结果表明,当偏转角为0°时,底板上的冷壁热通量相对较小,先是逐渐减小,其次在舵杆上沿流向最高。另一方面,当偏转角大于0°时,基板上的冷壁热通量迅速增加,尤其是对于舵杆上的冷壁热通量,随着温度的升高,冷壁热通量和基板上的静压变得越来越大。由于方向舵表面和板的相互作用,挠度增加了。同时,在相同水平位置处,发现在舵柱上的冷壁热通量与在舵的前缘上的冷壁热通量之比具有不同的总焓。

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