首页> 外文会议>Asia-Pacific international symposium on aerospace technology;APISAT 2010 >Experiment Investigation of Side Wall Boundary-Layer Blowing Control System of A Multi-element Airfoil Model in Wind Tunnel
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Experiment Investigation of Side Wall Boundary-Layer Blowing Control System of A Multi-element Airfoil Model in Wind Tunnel

机译:风洞中多元素翼型模型侧壁边界层吹气控制系统的试验研究

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The blowing control system of sidewall boundary layer in the NF-3 wind tunnel two dimensional sections and testing method were introduced in this paper. The control effect of wind tunnel side wall boundarylayer with different blowing coefficient and the effect of experiment result on aerodynamic characteristics of the high-lift airfoil were given. The results of initial experiment show that the system can effectively control the wind tunnel side wall boundary-layer, improve the lift coefficient We can conclude from this experiment that this control methodologycan effectively reduce the interference of side wall boundary-layer and improve the flow behavior of wind tunnel and the two dimension flowing characteristic over the airfoiL At last, the NF-3 wind tunnel experiment result and literature were compared for the sake of further verifying the effective of the NF-3 wind tunnel side wall boundarylayer blowing control system. It shows that this control system can effectively reduce the interference of wind tunnel side wall layer.
机译:介绍了NF-3风洞二维截面侧壁边界层的吹塑控制系统及测试方法。给出了不同吹气系数的风洞侧壁边界层的控制效果以及实验结果对高升力翼型气动特性的影响。初步实验结果表明,该系统可以有效地控制风洞侧壁边界层,提高升力系数。从本实验可以得出结论,该控制方法可以有效减少侧壁边界层的干扰,改善流动性最后,比较了NF-3风洞的实验结果和文献资料,以进一步验证NF-3风洞侧壁边界层吹扫控制系统的有效性。结果表明,该控制系统可以有效降低风洞侧壁层的干扰。

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