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Investigating the feedback path in a jet-surface resonant interaction

机译:研究射流表面共振相互作用中的反馈路径

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A resonant interaction between an 8:1 aspect ratio rectangular jet and flat-plates, placed parallel to the jet, is studied experimentally. For certain locations of the plate relative to the jet, the resonance takes place with a loud accompanying tone. The sound pressure level spectra are often marked by multiple peaks. The frequencies of the spectral peaks are studied as a function of the streamwise length of the plate, its relative location to the jet, and the jet Mach number. It is demonstrated that the tones are not due to a simple feedback between the plate's trailing edge and the nozzle's exit; the leading edge of the plate also comes into play in the frequency selection. With parametric variation, it is found that there is an order in the most energetic spectral peaks; their frequencies cluster in distinct bands. The 'fundamental' (i.e., the lowest) frequency band is explained by an acoustic feedback involving diffraction at the plate's leading edge.
机译:实验研究了长宽比为8:1的矩形射流与平行于射流放置的平板之间的共振相互作用。对于板相对于射流的某些位置,共振伴随着响亮的声音发生。声压级谱通常由多个峰标记。光谱峰值的频率是根据板的沿流方向的长度,板与射流的相对位置以及射流马赫数的函数进行研究的。事实证明,音调不是由于板的后缘和喷嘴的出口之间的简单反馈引起的。板的前沿也参与了频率选择。通过参数变化,发现在最高能谱峰中存在一个顺序;它们的频率聚集在不同的频带中。 “基本的”(即最低的)频带由涉及板的前缘处的衍射的声反馈来解释。

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