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首页> 外文期刊>Physics of fluids >Coherent structures in plasma-actuator controlled supersonic jets: Axisymmetric and mixed azimuthal modes
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Coherent structures in plasma-actuator controlled supersonic jets: Axisymmetric and mixed azimuthal modes

机译:等离子体致动器控制的超声速射流中的相干结构:轴对称和混合方位角模式

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摘要

High-fidelity simulations are employed to study the effect of eight localized arc filament plasma actuators placed around the periphery of a Mach 1.3 converging-diverging nozzle exit. Emphasis is placed on understanding the coherent structures generated by axisymmetric (m = 0), flapping or first mixed (m = ±1) and second mixed (m = ±2) modes, which are excited at the jet column-mode frequency corresponding to a Strouhal number based on jet diameter of 0.3. Baseline (no control) and constant excitation (actuators on continuously) cases are also simulated. Comparisons with experimental results indicate that the computational model reproduces the main features induced by the actuators. Furthermore, the mean flow exhibits many similarities with the theoretical predictions of Cohen and Wygnanski [J. Fluid Mech. 176, 221 (1987)]. Overall, the results indicate a complex coherent structure generation, evolution, and disintegration process. For m = ±1, the phase-averaged flow reveals successive distorted elliptic vortex rings with axes in the flapping plane but alternating on either side of the jet axis. This generates a chain of structures each of which interacts with its predecessor on one side of the major plane and its successor on the other. Through self and mutual induction, the leading segment of each loop is pinched and passes through the previous ring before rapidly breaking up. The m = ±2 mode yields elliptic structures with major axes of successive rings being aligned with the two symmetry planes, which are orthogonal to each other. The minor axis side is pulled downstream faster than the rest of the structure because of the higher velocity near the jet centerline and self-induced effects, yielding a horse-shoe shape when viewed in profile. The m = 0 mode exhibits axisymmetric roll-up events, with vortex ribs in the braid regions connecting successive large coherent structures. The constant excitation (with largest energy input) and baseline cases are similar to each other, indicating that the direct effect of heating is negligible.
机译:高保真模拟用于研究在1.3马赫会聚-发散喷嘴出口周围布置的八个局部电弧丝等离子体致动器的效果。重点放在理解由轴对称(m = 0),拍打或第一混合(m =±1)和第二混合(m =±2)模式产生的相干结构,这些模式在与Strouhal数基于喷嘴直径0.3。还模拟了基线(无控制)和恒定励磁(执行器连续运行)情况。与实验结果的比较表明,该计算模型再现了由执行器引起的主要特征。此外,平均流量显示出与Cohen和Wygnanski的理论预测有很多相似之处[J.流体机械。 176,221(1987)]。总的来说,结果表明一个复杂的,连贯的结构生成,演化和分解过程。当m =±1时,相位平均流显示出连续的扭曲椭圆形涡流环,其轴在拍打平面中,但在射流轴的任一侧交替出现。这样就产生了一系列结构,每个结构在主平面的一侧与它的前任交互,在另一平面与它的后继交互。通过自感应和互感应,每个环的前导段都会被挤压并穿过前一个环,然后迅速分解。 m =±2模式产生椭圆结构,其连续环的主轴线与两个正交的对称平面对齐。由于靠近射流中心线的较高速度和自感应效应,短轴侧比结构其余部分更快地向下游拉动,从侧面看时会产生马蹄形的形状。 m = 0模式表现出轴对称的卷起事件,编织区域中的涡旋肋连接了连续的大相干结构。恒定激励(具有最大能量输入)和基线情况彼此相似,表明加热的直接影响可以忽略不计。

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