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Interaction of a flow-excited Helmholtz resonator with a grazing turbulent boundary layer

机译:激流亥姆霍兹共振器与掠掠湍流边界层的相互作用

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摘要

This study focuses on the characteristics of the flow oscillations induced by various Helmholtz resonators which are excited by a fully developed turbulent grazing flow. A full experimental investigation has been conducted in a subsonic wind tunnel with a low turbulence level. Detailed fluid dynamic and acoustic analyses of the flow inside the wall-mounted resonator and within the shear layer have been performed. The results reveal that the degree of excitation of the pressure and velocity fields is related to the resonator geometry, and that the pressure fluctuations within the resonator are most sensitive to the orifice length for the range of geometric parameters considered. Interestingly, the turbulent length scale over the orifice with the minimum diameter was found to be higher than the other cases investigated. This in turn causes a modification to the turbulent structures downstream of the resonator. The turbulence intensity and energy spectra of the velocity fluctuations within the turbulent boundary layer downstream of the resonators demonstrate that in a specific velocity range certain resonators have the potential to modify the flow instabilities within the turbulent boundary layer. The results provide information on the relationship between the pressure and velocity fluctuations within and downstream of the resonator and the geometric characteristics of the resonator and the properties of the grazing flow.
机译:这项研究的重点是由各种亥姆霍兹共振器引起的流动振荡的特性,这些振动被充分发展的湍流掠流激发。在湍流度低的亚音速风洞中进行了全面的实验研究。已对壁挂式谐振器内部和剪切层内部的流动进行了详细的流体动力学和声学分析。结果表明,压力场和速度场的激发程度与谐振器的几何形状有关,并且对于所考虑的几何参数范围,谐振器内的压力波动对孔口长度最为敏感。有趣的是,发现在最小直径的孔口上的湍流长度尺度高于其他研究情况。这进而导致对谐振器下游的湍流结构的修改。谐振器下游湍流边界层内速度波动的湍流强度和能谱表明,在特定速度范围内,某些谐振器具有改变湍流边界层内流动不稳定性的潜力。结果提供了关于谐振器内部和下游的压力和速度波动与谐振器的几何特性以及掠流特性之间的关系的信息。

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