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Investigation of noise sources in high-speed jets via correlation measurements

机译:通过相关测量研究高速喷气机中的噪声源

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To locate noise sources in high-speed jets, the far-field sound pressure fluctuations p' were correlated with each of density rho, axial velocity u, radial velocity v, rho uu and rho vv fluctuations measured from various points in jet plumes. Detailed surveys were conducted in fully expanded, unheated plumes of Mach 0.95, 1.4 and 1.8. The velocity and density fluctuations were measured simultaneously using a recently developed non-intrusive point measurement technique based on molecular Rayleigh scattering. The technique uses a continuous-wave narrow line-width laser, Fabry-Perot interferometer and photon counting electronics. Laser light scattered by air molecules from a 1.06 mm long region on the narrow beam was collected and spectrally resolved by the interferometer. It was observed that the fluctuation spectra for air density inside the plume were in general similar to those of axial velocity spectra, while the radial velocity spectra were somewhat different. For the correlation study, microphone polar angles were varied from 30 degrees to 90 degrees to the jet axis. The sound pressure fluctuations p, at the shallowest 30 degrees angle provided the highest correlation with turbulent fluctuations. The correlations sharply decreased as the polar angle was increased to 60 degrees, beyond which all data mostly fell below the experimental noise floor. Among all turbulent fluctuations correlations showed the highest values. Correlation with the first-order terms , and third-order terms was higher than that from the second-order terms <(rho) over baru'u'; p'> and <(u) over bar rho'u'; p'>. Both < v'; p'> and correlations with the 90 degrees microphone signal fell below the experimental noise floor, while that from the shallow 30 degrees microphone showed weaker values. By moving the laser probe to various locations in the jet, it was found that the strongest noise source lay downstream of the end of the potential core and extended many diameters beyond. Correlation measurements from turbulent fluctuations along the lip shear layer showed a Mach-number dependency: significant values were measured in supersonic jets, while correlations fell below the noise floor for subsonic jets. Various additional analyses showed that fluctuations from large coherent structures mostly contributed to the measured correlation, while that from small-scale structures fell below the noise floor.
机译:为了定位高速喷气机中的噪声源,将远场声压波动p'与从射流羽流各个点测得的密度rho,轴向速度u,径向速度v,rho uu和rho vv波动相关。详细的调查是在0.95、1.4和1.8马赫的完全膨胀,未加热的烟羽中进行的。使用最近开发的基于分子瑞利散射的非侵入点测量技术,可以同时测量速度和密度波动。该技术使用连续波窄线宽激光器,法布里-珀罗干涉仪和光子计数电子设备。空气分子从窄束上1.06毫米长的区域散射的激光被收集并通过干涉仪进行光谱分辨。可以看出,羽流内部空气密度的波动谱通常与轴向速度谱相似,而径向速度谱则有所不同。对于相关性研究,麦克风的极角相对于喷射轴的角度从30度到90度不等。在最浅的30度角处的声压波动p与湍流波动的相关性最高。当极角增加到60度时,相关性急剧下降,超过此角度,所有数据大多降到实验本底噪声以下。在所有湍流波动中相关性显示出最高值。与一阶项和三阶项高于二阶项和<(u)超过bar rho'u'; p'>。均

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