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Investigation of Counter-Rotating Open-Rotor Orthogonal Blade/Vortex Interaction Noise

机译:反向旋转正交转子叶片/涡流相互作用噪声的研究

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This paper investigates the influence of vortex models on the noise radiated by the orthogonal interaction of a rotating blade with a prescribed vortex. The blade motion, the vortex maximum velocity and core radius are set to produce an interaction representative of the ones occurring on a counter-rotating open-rotor at takeoff condition where interaction noise is prominent. Different compressible vortex models are considered. Links are made between radiated noise and the vortex velocity profiles. It is shown that velocity decay in the free-vortex region has a strong impact on the noise radiated at low frequencies while the inner structure of the vortex influences the acoustic spectra content at high frequencies.
机译:本文研究了涡旋模型对旋转叶片与规定涡旋的正交相互作用所辐射的噪声的影响。叶片运动,涡旋最大速度和芯半径被设置为产生相互作用,该相互作用表示在相互作用噪声非常明显的起飞条件下在反向旋转的开放转子上发生的相互作用。考虑了不同的可压缩涡模型。在辐射噪声和涡流速度曲线之间建立了联系。结果表明,自由涡旋区的速度衰减对低频辐射的噪声有很大影响,而涡旋的内部结构会影响高频声谱的含量。

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