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A New Method of Controlling Cavity-induced Pressure Oscillations Using Sub-cavity

机译:利用子腔控制腔致压力振荡的新方法

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摘要

A new passive control technique of cavity-induced pressure oscillations has been investigated numerically for a supersonic two-dimensional flow over open rectangular cavities at Mach number 1.83 at the cavity entrance. A sub-cavity on the front wall of the cavity covered by a flat plate was evaluated for the effectiveness of controlling cavity-induced acoustic oscillations. The results showed that sub-cavity is very effective in reducing cavity-induced pressure oscillations. The results also showed that the resultant amount of attenuation of cavity-induced pressure oscillations was dependent on the length and thickness of the flat plate, and also on the depth of the sub-cavity used as an oscillation suppressor.
机译:在腔入口处马赫数为1.83的开放矩形腔上,通过超声速二维流动,对腔引起的压力振荡的一种新的被动控制技术进行了数值研究。评估了由平板覆盖的腔体前壁上的子腔体对控制腔体引起的声振荡的有效性。结果表明,亚型腔在减少型腔引起的压力波动方面非常有效。结果还表明,腔引起的压力振荡的衰减量取决于平板的长度和厚度,还取决于用作振荡抑制器的子腔的深度。

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