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Control of Flow Around Square Cylinders at Incidence by Using a Rod

机译:使用杆控制发生事故时方形气缸周围的流动

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Aerodynamic characteristics of a square cylinder at incidence were investigated experimentally in the wake of a small rod at a Reynolds number of 3.4 x 10~4. The dimensionless gap L/D was varied from 1.71 to 8.00. Depending on the spacing L/D, two flow patterns with and without vortex shedding from the rod were observed. Pressure measurements on the rod and square cylinder and hot-film measurements in the wake of the cylinder were carried out. The combined influences of the rod and angle of incidence on the pressure distributions and vortex-shedding phenomenon were investigated. Without the rod, as the incidence increases from 0 deg, the reattachment on the lower side surface of the square cylinder occurs at the vicinity of 13 deg, and this corresponds to a jump in the Strouhal number. However, when the rod was set upstream of the square cylinder, the reattachment occurs at smaller angles of incidence depending on L/D. At zero angle of incidence, the minimum value of drag on the square cylinder is obtained for L/D = 2.0 and produces a drag that is 30% that of the square cylinder without rod. For L/D = 1.71, with increasing the angle of incidence C_D values approximate to those of the square cylinder without rod. In the case of L/D ≥ 2.7, there is a considerable decrease in C_D in the region θ ≤ 10 deg; however, the effect of the rod on C_D decreases beyond θ= 10 deg.
机译:在雷诺数为3.4 x 10〜4的小棒后,通过实验研究了方形圆柱入射时的空气动力学特性。无量纲间隙L / D从1.71变化到8.00。取决于间距L / D,观察到有和没有从杆上涡流脱落的两种流动模式。进行了棒和方筒上的压力测量以及筒后的热膜测量。研究了杆和入射角对压力分布和涡流脱落现象的综合影响。在没有杆的情况下,随着入射角从0度开始增加,在方圆柱体下侧面的重新连接发生在13度附近,这对应于斯特劳哈尔数的跳跃。但是,当将杆放置在方形气缸的上游时,取决于L / D,重新连接会以较小的入射角发生。在零入射角下,对于L / D = 2.0,将获得方筒上的最小阻力值,并且产生的阻力是不带杆的方筒的30%。当L / D = 1.71时,随着入射角的增加,C_D值近似于不带杆的方形圆柱的值。在L / D≥2.7的情况下,在θ≤10度的区域C_D明显降低;但是,杆对C_D的影响会减小到θ= 10度以上。

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