论文标题
在合成喷气机的涡旋动力学上 - 湍流边界层相互作用
On the vortex dynamics of synthetic jet -- turbulent boundary layer interactions
论文作者
论文摘要
通过使用立体粒子图像速度法(SPIV)对合成射流与湍流边界层的相互作用相互作用产生的涡流动力学进行了研究。测试了三个纵横比18矩形孔的几何形状,包括向墙壁发出正常发出的跨度和面向流向的孔口,并以跨度为导向的孔口向下游投入$ 45^\ circ $。此外,测试了三个驱动条件,以探索吹击比和曲路数字的影响。在一系列测量平面上获得的SPIV数据用于重建三维平均值和相锁的速度场,从而对涡流的形成和开发进行了详细的分析。孔口几何形状和流量条件的变化产生了一系列涡流结构,包括扭曲的涡旋环,发夹涡旋和拱形涡流。来自壁正常孔的喷射器以与边界层涡流旋转相同的方向旋转的涡旋支配,从而通过增加混合来增强近壁流速。相反,俯仰喷气机中的主要结构旋转到边界层涡度,这些喷气机通过直接动量增加了壁附近的流速。流场分析表明,合成的喷射层相互作用导致以低吹式比率运行的倾斜喷射,从而产生优势涡流,这些涡流比在相同条件下由壁正态喷射物产生的涡流弱得多。最后,在最低的曲线数测试了壁正常喷气机中的涡旋之间的间距增加的间距增加,导致不稳定的混合比在较高的曲霉数下观察到的要高得多。
The vortex dynamics resulting from the interaction of synthetic jets with turbulent boundary layers was investigated experimentally using stereoscopic particle image velocimetry (SPIV). Three aspect ratio 18 rectangular orifice geometries were tested including spanwise and streamwise-oriented orifices issuing normal to the wall and a spanwise-oriented orifice pitched $45^\circ$ downstream. Additionally, three actuation conditions were tested to explore the impact of varying blowing ratio and Strouhal number. SPIV data obtained on an array of measurement planes was used to reconstruct the three-dimensional mean and phase-locked velocity fields, enabling detailed analysis of the formation and development of the vortices. The variations in the orifice geometry and the flow conditions produced a range of vortex structures including distorted vortex rings, hairpin vortices, and arch-shaped vortices. The jets from wall-normal orifices were dominated by vortices that rotated in the same direction as the boundary layer vorticity which enhanced the near-wall flow velocity by increasing mixing. Conversely, the dominant structures in the pitched jets rotated counter to the boundary layer vorticity, and these jets enhanced the flow velocity near the wall through direct momentum addition. Flow field analysis revealed that the synthetic jet-boundary layer interaction caused pitched jets operated at low blowing ratios to produce dominant vortices which were much weaker than those generated by wall-normal jets at the same conditions. Finally, at the lowest Strouhal number tested the increased spacing between the vortices in the wall-normal jets resulted in much higher unsteady mixing than was observed at higher Strouhal numbers.