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伯拉克·图尔汗;王志进;伊斯梅特·古苏尔

周期性俯冲翼型非定常尾迹的相干性。 （英语） Zbl 1524.76164号

J.流体力学。 938，论文编号A14，32 p.（2022）.
小结：我们对NACA0012翼型在弦雷诺数为（Re=20000）和基于峰间振幅（St）的降低频率（k）和Strouhal数的宽范围内正弦下落的近尾迹流动结构进行了实验研究。使用平均速度场和脉动速度场估算的平均推力系数证实了（St^2）相关性以及（k\leq 1）降低频率的显著影响。通常，在测试范围内（k\leq 3.14和St\leq 0.24），时间平均流量与（St）的相关性比与（k）的相关性更好。使用两点互相关和适当的正交分解对近尾流中的顺流和交叉流进行分析，结果表明，非定常特性与\（St）的相关性甚至比与平均流量的相关性更好。顺流基本尾迹模式和横流拍动模式的能量百分比随着St的增加而增加，但在拖曳尾迹和推力尾迹中以不同的速率增加。与振荡物体后面的尾迹同步有相似之处。对于较小的（St）（在产生阻力的尾迹中），测量域中的展向平均互相关系数线性增长，对于较大的（St）（在推力产生的尾迹），该系数几乎恒定在较高的值。结果表明，Strouhal数是决定尾迹二维度的最重要参数，表明翼展方向的涡在St geq 0.05和x/c leq 4下是准二维的。讨论了使用振荡翼型的实验阵风发生器的意义。

引用于1文件

MSC公司：

76D25型 尾迹和喷流
76D17号 粘性涡流
76B10型 射流和空腔、空化、自由流线理论、进水问题、翼型和水翼理论、晃动

关键词：

漩涡街道;唤醒
PDF格式BibTeX公司 XML格式引用
\textit{B.Turhan}等人，《流体力学杂志》。938，论文编号A14，32页（2022；Zbl 1524.76164）
全文： 内政部 链接

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此参考列表基于出版商或数字数学图书馆提供的信息。其项与zbMATH标识符进行启发式匹配，可能包含数据转换错误。在某些情况下，zbMATH Open的数据对这些数据进行了补充/增强。这试图尽可能准确地反映原始论文中列出的参考文献，而不要求完整或完全匹配。