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Modification of vortex dynamics and transport properties of transitional axisymmetric jets using zero-net-mass-flux actuation

机译:零净质量通量激励对过渡轴对称射流涡流动力学和输运特性的修正

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We study the near field of a zero-net-mass-flux (ZNMF) actuated round jet using direct numerical simulations. The Reynolds number of the jet Re_D = 2000 and three ZNMF actuators are used, evenly distributed over a circle, and directed towards the main jet. The actuators are triggered in phase, and have a relatively low momentum coefficient of C_μ = 0.0049 each. We study four different control frequencies with Strouhal numbers ranging from St_D = 0.165 to StD = 1.32; next to that, also two uncontrolled baseline cases are included in the study. We find that this type of ZNMF actuation leads to strong deformations of the near-field jet region that are very similar to those observed for non-circular jets. At the end of the jet's potential core (x/D = 5), the jet-column cross section is deformed into a hexagram-like geometry that results from strong modifications of the vortex structures. Two mechanisms lead to these modifications, i.e., (i) self-deformation of the jet's primary vortex rings started by distortions in their azimuthal curvature by the actuation, and (ii) production of side jets by the development and subsequent detachment of secondary streamwise vortex pairs. Further downstream (x/D = 10), the jet transforms into a triangular pattern, as the sharp corner regions of the hexagram entrain fluid and spread. We further investigate the global characteristics of the actuated jets. In particular when using the jet preferred frequency, i.e., St_D = 0.33, parameters such as entrainment, centerline decay rate, and mean turbulent kinetic energy are significantly increased. Furthermore, high frequency actuation, i.e., StD = 1.32, is found to suppress the mechanisms leading to large scale structure growth and turbulent kinetic energy production. The simulations further include a passive scalar equation, and passive scalar mixing is also quantified and visualized.
机译:我们使用直接数值模拟研究零净质量通量(ZNMF)驱动的圆形射流的近场。喷嘴Re_D = 2000的雷诺数和三个ZNMF执行器被使用,均匀分布在一个圆上,并指向主喷嘴。执行器是同相触发的,并且每个驱动器具有相对较低的动量系数C_μ= 0.0049。我们研究了Strouhal数从St_D = 0.165到StD = 1.32的四个不同的控制频率;其次,还包括了两个不受控制的基线案例。我们发现,这种ZNMF致动导致近场射流区域的强烈变形,这与非圆形射流所观察到的非常相似。在射流的潜在核心末端(x / D = 5),射流柱的横截面变形为六角形几何形状,这是涡流结构的强烈变化所致。两种机制导致了这些修改,即(i)射流主涡流环的自变形是由致动引起的其方位角曲率的扭曲开始的;以及(ii)通过产生和随后分离次级流向涡流而产生了副射流。对。在更下游(x / D = 10),当六边形的尖角区域夹带流体并扩散时,射流转变为三角形。我们进一步研究了驱动射流的整体特性。特别是当使用喷射器的优选频率,即St_D = 0.33时,诸如夹带,中心线衰减率和平均湍动能之类的参数显着增加。此外,发现高频致动,即StD = 1.32,抑制了导致大规模结构增长和湍动能产生的机制。模拟还包括一个无源标量方程,并且还对无源标量混合进行了量化和可视化。

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