首页> 外文会议>Congress of the International Council of the Aeronautical Sciences;International Council of the Aeronautical Sciences >INFLUENCE OF WING ASPECT RATIO ON PASSIVE STALL CONTROL AT LOW REYNOLDS NUMBER USING SINUSOIDAL LEADING EDGES
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INFLUENCE OF WING ASPECT RATIO ON PASSIVE STALL CONTROL AT LOW REYNOLDS NUMBER USING SINUSOIDAL LEADING EDGES

机译:翼展比对正弦前缘在低雷诺数下被动失速控制的影响

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The SST k-ω DDES model has been used tostudy the influence of wing aspect ratio onpassive stall control at low Reynolds numberusing sinusoidal leading edges. Both stalled andunstalled flow conditions were considered toanalyze the effect of low Reynolds numbercorrections on the performance of the DDESmodel. It was concluded that major improvementsto the foregoing correction are stillrequired to deal with stalled flow conditions andtwo proposals have been investigated as well.
机译:SSTk-ωDDES模型已用于 研究机翼长宽比对机翼的影响 雷诺数低时的被动失速控制 使用正弦曲线的前缘。都停滞了 不稳定的流动条件被认为是 分析低雷诺数的影响 DDES性能的更正 模型。结论是重大改进 对上述纠正仍 需要处理停滞的流量条件,以及 还研究了两个建议。

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