Small-width wall-attached Coandǎ jets for flow control

IF 2.8 Q2 MECHANICS Flow (Cambridge, England) Pub Date : 2023-06-16 DOI:10.1017/flo.2023.9
Oussama El Mokkadem, Xintong Chen, Charlene Phan, J. Delva, P. Joseph, A. Dazin, F. Romanò
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Abstract

Abstract The flow dynamics of small-width wall-attached jets generated by a Coand-effect nozzle is investigated by unsteady Reynolds-averaged Navier–Stokes simulations. The data are validated by comparison with hot-wire velocity measurements performed on the same flow configurations. The jets exhibit a complex topology strongly influenced not only by the spanwise vorticity (as usually observed in wall jets) but also by a vorticity component normal to the wall and induced by the shear layer developing on the jet sides. This results in an original U-shaped jet whose characteristics are studied in detail for three different mass flow rates. The robustness of the flow topology on a larger range of injected mass flow rates is finally presented and discussed in terms of the injected momentum near the wall. The resulting flow profiles point out that our injector is expected to be a promising candidate for active flow control in gas-turbine compressors for aeronautical and energy applications.
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用于流动控制的小宽度壁挂式喷管
摘要采用非定常reynolds -average Navier-Stokes模拟方法研究了coand效应喷管产生的小宽度附壁射流的流动动力学。通过与在相同流体配置下进行的热线速度测量进行比较,验证了数据的有效性。射流表现出复杂的拓扑结构,不仅受到展向涡度(通常在壁面射流中观察到)的强烈影响,而且受到垂直于壁面的涡度分量的强烈影响,这是由射流两侧形成的剪切层引起的。这就得到了一个原始的u形射流,在三种不同的质量流量下,对其特性进行了详细的研究。最后给出了流动拓扑在较大注入质量流量范围内的鲁棒性,并从壁面附近注入动量的角度进行了讨论。由此得到的流动曲线表明,我们的喷射器有望成为航空和能源领域燃气涡轮压气机主动流动控制的有希望的候选者。
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