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Synthetic Jets in Crossflow

机译:横流中的合成射流

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Results of an experimental investigation on synthetic jets, with and without crossflow, from orifices of different geometry are presented. Jet Reynolds number up to 2.3 x 10~4 and Stokes number up to 400 are covered. For the round orifice, in the absence of crossflow, the threshold for formation of the synthetic jet is found to be at a stroke length, L_0/D ≈ 0.25. Above L_0/D ≈ 5, the profiles of normalized centerline mean velocity appear to become invariant. It is reasoned that the limiting behavior at high L_0/D is related to the phenomenon of saturation of impulsively generated vortices. For the synthetic jet in crossflow (SJCF), distributions of mean velocity, stream wise vorticity, as well as turbulence intensity are found to be similar to those of a steady jet-in-crossflow (JICF). A pair of counter-rotating streamwise vortices, corresponding to the bound vortex pair of the steady case, is clearly observed. Mean velocity field, for the case of normal injection, exhibits a "dome" of low-momentum fluid pulled up from the boundary layer, and the entire domain is characterized by high turbulence. When the maximum velocity during the discharge stroke of a SJCF equals the exit velocity of a JICF, the penetration of the two are found to be comparable for a given crossflow. Other orifice geometries included a tapered, a pitched, and a cluster of nine, all having the same cross-sectional area at the exit. The flowfield from the cluster, when viewed a few equivalent diameters downstream, resembles that from the single orifice. However, jet penetration is somewhat lower as a result of increased mixing of the distributed jets with the crossflow. Instead of the dome of low-momentum fluid, a pitched SJCF is characterized by a core of high-momentum fluid. Its penetration is the lowest, as expected. The trajectory of the SJCF from a single orifice, normal or pitched, is well represented by the power function correlation available for a JICF.
机译:给出了来自不同几何形状孔口的有或没有横流的合成射流的实验研究结果。包括雷诺数达2.3 x 10〜4和斯托克斯数达400。对于圆形孔口,在没有错流的情况下,发现合成射流的形成阈值为冲程长度L_0 / D≈0.25。在L_0 / D≈5以上,归一化的中心线平均速度分布似乎变得不变。有理由认为,在高L_0 / D时的限制行为与脉冲产生的旋涡的饱和现象有关。对于横流式合成射流(SJCF),平均速度,水流涡度以及湍流强度的分布与稳定的横流式射流(JICF)相似。可以清楚地观察到一对反向旋转的涡流,它们对应于稳定情况的束缚涡对。对于正常注入的情况,平均速度场表现出从边界层拉起的低动量流体的“圆顶”,并且整个区域的特征是高湍流。当SJCF的排出冲程期间的最大速度等于JICF的出口速度时,对于给定的横流,发现两者的渗透率相当。其他孔的几何形状包括锥形,螺距和九个簇,它们在出口处均具有相同的横截面积。当从下游观察几个等效直径时,来自簇的流场类似于来自单个孔口的流场。但是,由于分配的射流与错流的混合增加,射流的穿透力会有所降低。倾斜的SJCF代替了低动量流体的穹顶,其特点是高动量流体的核心。正如预期的那样,它的渗透率是最低的。来自单个孔口(正常或倾斜)的SJCF的轨迹很好地代表了JICF的幂函数相关性。

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