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An Experimental Study Synthetic Jets from Rectangular Orifices

机译:矩形孔口合成射流的实验研究

摘要

Results of an experimental investigation on isolated synthetic jets in crossflow from rectangular orifices of different aspect ratio and orientation are presented. Three aspect ratios, AR = 4, 8, and 16, with pitch a = 90deg., were investigated, Additionally, the AR = 8 case was pitched at 20 deg.. The yaw angle, , was varied through 0 deg., 10 deg., 45 deg. and 90 deg.. All orifices had same exit area and the data were compared with synthetic as well as steady jet from a circular orifice of same area. Hotwire measurements were performed to obtain all three components of mean velocity and turbulent stresses. Data were acquired for momentum-flux ratio up to J = 50. Distributions of time- and phase-averaged data were obtained on the cross sectional plane at x/D = 0.5, 5 and 10, as well as on the axial plane of the symmetry. Qualitative flowfield similarity between synthetic and steady jets is observed. However, high-momentum 'cap' above the low-momentum 'dome', characteristic of steady jets, does not necessarily appear in the synthetic jet. The position and shape of the high-momentum region depend on the distance from the orifice, pitch, yaw as well as momentum-flux ratio. Consequently, the location of the minimum velocity in the 'dome' measured at the plane of symmetry, y(submin), is adopted as a reference for penetration estimate and trajectory comparison. For AR = 16, the dome is the largest in area with maximum velocity deficit. However, the penetration is somewhat higher for AR = 4. Increase in yaw reduces the spatial extent of the dome and the penetration height but augments the velocity deficit. At low J the dome is connected to the boundary layer and traces of the cap of high momentum fluid are visible above it. Increase in J lifts the dome and reorganizes the high-momentum fluid around its perimeter, eventually bringing it underneath. Phase-averaged data document dynamic topological changes within the cycle. Phase-averaged streamwise velocity contours on the cross-sectional plane exhibit behavior commensurate with that seen in time-averaged data at various J.
机译:提出了对不同纵横比和方向的矩形孔进行横流分离的合成射流的实验研究结果。研究了三个高宽比,AR = 4、8和16,俯仰a = 90度。此外,AR = 8情况下俯仰角为20度。偏航角α改变了0度,即10度度,45度90°和90°。所有孔具有相同的出口面积,并且将数据与来自相同面积的圆形孔的合成以及稳定射流进行比较。进行热线测量以获得平均速度和湍流应力的所有三个分量。获得的动量与通量之比的数据不超过J =50。在x / D = 0.5、5和10的横截面上,以及在轴的轴向上,获得时间和相位平均数据的分布。对称。观察到合成射流与稳定射流之间的定性流场相似性。但是,稳定射流特有的低动量“圆顶”上方的高动量“上限”不一定会出现在合成射流中。高动量区域的位置和形状取决于与孔的距离,螺距,偏航角以及动量-通量比。因此,在对称面y(submin)上测得的“穹顶”中的最小速度位置被用作穿透估计和轨迹比较的参考。对于AR = 16,穹顶面积最大,速度不足。但是,AR = 4时,穿透力会更高。偏航的增加会减小圆顶的空间范围和穿透高度,但会增加速度不足。在低J处,圆顶连接到边界层,并且在其上方可以看到高动量流体盖的痕迹。 J的增加会抬起球罩,并在其周边重新组织高动量流体,最终将其带到下方。相平均数据记录了周期内的动态拓扑变化。横截面上的相位平均流向速度轮廓与在各种J下的时间平均数据中看到的行为相称。

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