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首页> 外文期刊>Journal of Sound and Vibration >NOISE FROM SUPERSONIC COAXIAL JETS .3. INVERTED VELOCITY PROFILE
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NOISE FROM SUPERSONIC COAXIAL JETS .3. INVERTED VELOCITY PROFILE

机译:超音速飞机噪声3。速度分布图

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摘要

The instability wave noise generation model is used to study the instability waves in the two shear layers of an inverted velocity profile, supersonic, coaxial jet and the noise radiated from the dominant wave. The inverted velocity profile jet has a high speed outer stream surrounding a low speed inner stream and the outer shear layer is always larger than the inner shear layer. The jet mean flows are calculated numerically. The operating conditions are chosen to exemplify the effect of the coaxial jet outer shear layer initial spreading rates. Calculations are made for the stability characteristics in the coaxial jet shear layers and the noise radiated from the instability waves for different operating conditions with the same total thrust, mass flow and exit area as a single reference jet. Results for inverted velocity profile jets indicate that relative maximum instability wave amplitudes and far held peak noise levels can be reduced from that of the reference jet by having higher spreading rates for the outer shear layer, low velocity ratios, and outer streams hotter than the inner stream. (C) 1997 Academic Press Limited. [References: 22]
机译:失稳波噪声产生模型用于研究速度分布反转,超音速,同轴射流的两个剪切层中的失稳波以及从主波辐射的噪声。反向速度分布射流具有围绕低速内部流的高速外部流,并且外部剪切层始终大于内部剪切层。射流平均流量通过数值计算。选择操作条件以举例说明同轴射流外剪切层初始铺展速率的影响。计算同轴射流剪切层的稳定性特征,以及在不同的工况下从不稳定性波辐射出的噪声,这些噪声具有与单个参考射流相同的总推力,质量流量和出口面积。反向速度剖面射流的结果表明,相对于参考射流,相对最大不稳定波幅值和保持较远的峰值噪声水平可以通过使外剪切层的扩散速率更高,速度比低并且外流比内层更热而降低流。 (C)1997 Academic Press Limited。 [参考:22]

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