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Active control of coaxial jet mixing with manipulation of primary vortical structures by arrayed micro flap actuators

机译:主动控制同轴射流混合,并通过阵列微风门执行器操纵初级涡旋结构

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摘要

Active mixing control of a methane/air isothermal coaxial jet was achieved using micro magnetic flap actuators arranged on the inner surface of the outer annular nozzle. The spatio-temporal evolution of vortical structures and the scalar mixing were studied through the particle image velocimetry and planar laser-induced fluorescence methods. In contrast to studies on jet control using acoustic forcing, the mechanical movement of the flap directly generated large-scale intense vortices. The mixing was enhanced significantly by the vortices formed in the inner shear layer, although the control input was given to the outer shear layer. It was found that the primary vortex rings dominated the near-field mixing, while streamwise vortices were responsible for the downstream mixing. It was also demonstrated that the radial range of the inner fuel transportation could be manipulated flexibly by adjusting the shedding interval of the vortices. Especially, the mixing was enhanced most significantly when the primary vortices were most densely populated near the nozzle exit at the control Strouhal number of unity.
机译:甲烷/空气等温同轴射流的主动混合控制是通过使用布置在外部环形喷嘴内表面上的微磁瓣执行器来实现的。通过粒子图像测速和平面激光诱导荧光方法研究了旋涡结构的时空演化和标量混合。与使用声强迫进行射流控制的研究相反,襟翼的机械运动直接产生大规模的强烈涡旋。尽管将控制输入提供给了外部剪切层,但内部剪切层中形成的涡旋显着增强了混合。发现初级涡流环主导了近场混合,而流向涡旋则负责下游混合。还证明了通过调节涡流的脱落间隔可以灵活地控制内部燃料输送的径向范围。尤其是,当初级旋涡在喷嘴出口附近以控制Strouhal单位数最密集时,混合最明显地增强。

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