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The Evaluation of Drag and Lift Force of Groove Cylinder in Wind Tunnel

机译：风洞槽圆筒拖曳力的评价

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Wan Mohamad Aiman Wan Yahaya; Syahrullail Samion; Fazila Mohd Zawawi; Mohd Nor Musa; Muhammad Naim Aiman Najurudeen;
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1. Wind tunnel tests for mean drag and lift coefficients on multiple circular cylinders arranged in-line [J] . Liu XZ, Levitan M, Nikitopoulos D Journal of Wind Engineering and Industrial Aerodynamics: The Journal of the International Association for Wind Engineering . 2008,第6a7期

机译：风洞测试用于串联排列的多个圆柱上的平均阻力和升力系数
2. Optimum driving condition for lift creating cylinder by plasma actuators based on wind tunnel evaluation-based design [J] . Masahiro Kanazaki, Takashi Matsuno, Kengo Maeda, International Journal of Automation and Logistics . 2016,第1a2期

机译：基于风洞评估的等离子致动器产生升力缸的最佳驱动条件
3. Drag and lift forces on a stationary cylinder in a linear shear flow at a low Reynolds number [J] . Liu Jiabin, Bai Xiaodong, Guo Anxin Journal of Fluids and Structures . 2020,第期

机译：在低雷诺数的线性剪切流动中拖动力量
4. Lift and drag forces on a cylinder in the wake of an upstream cylinder [C] . Wusheng Wu, Shan Huang, Nigel Barltrop International conference on offshore mechanics and arctic engineering;OMAE'99 . 2000

机译：在上游气缸之后，气缸上的提升力和阻力
5. An investigation of the effect of a varying boundary layer on the lift and drag coefficients of a circular cylinder next to a solid boundary. [D] . Chavez, Manuel. 1969

机译：研究边界层变化对紧邻实心边界的圆柱体的升力和阻力系数的影响。
6. Wind Tunnel Measurement Systems for Unsteady Aerodynamic Forces on Bluff Bodies: Review and New Perspective [O] . Zengshun Chen, Yemeng Xu, Hailin Huang, 2020

机译：虚空隧道测量系统在虚空体上为不稳定的空气动力力量：审查和新的视角
7. Measurements of the pressure distributions on two circular cylinders of diameter d, vertically immersed in a turbulent boundary layer, are performed for various cylinder spacings s and angles of attack φ. The characteristics of the drag and lift forces acting on the cylinder are classified into three regions : i.e., 1) 0°＜__〜φ＜__〜30°, 2) 30°＜__〜φ＜__〜120°and 3) 120°＜__〜φ＜__〜180°which are divided by the two zero-lift force lines. Moreover, it is found that the interference between two cylinders is almost negligible for s/d＞__〜4, except for the influence of the wake region of the upstream cylinder. [O] . 谷口清一, 坂本弘志, Seiichi TANIGUCHI, 1980

机译：对于不同的气缸间距s和迎角φ，对垂直浸入湍流边界层的直径为d的两个圆柱上的压力分布进行测量。作用在气缸上的阻力和提升力的特性分为三个区域：1）0°＜__ 〜φ ＜__ 〜30°，2）30°＜__ 〜φ ＜__ 〜120°和3） 120°＜__ 〜φ ＜__ 〜180°除以两条零升力线。而且，发现除了上游气缸的尾流区域的影响之外，对于s / d＞ __〜4，两个气缸之间的干扰几乎可以忽略。

The Evaluation of Drag and Lift Force of Groove Cylinder in Wind Tunnel

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