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A numerical study on the effects of design parameters on the acoustics noise of a high efficiency propeller

机译:设计参数对高效螺旋桨声学噪声影响的数值研究

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Purpose A numerical study on the aerodynamic noise generation of a high efficiency propeller is carried out.Design/methodology/approach Three-dimensional numerical simulation based on Reynolds averaged N-S model is performed to obtain the aerodynamic performance of the propeller. Then, the result of the aerodynamic analysis is given as input of the acoustic calculation. The sound is calculated using the Farassat 1A which was derived from Ffowcs Williams-Hawkings equation and is compared with the measurements.Findings Moreover, the fan is modified for noise reduction by changing its geometrical parameters such as span, chord length and torsion angle.Originality/value The variation trend of aerodynamic and acoustic are compared and discussed for different modification tasks. Some meaningful conclusions are drawn on the noise reduction of propeller.
机译:目的对高效螺旋桨的空气动力噪声进行数值研究。设计/方法/方法基于雷诺兹平均N-S模型进行三维数值模拟,以获得螺旋桨的空气动力性能。然后,将空气动力学分析的结果作为声学计算的输入。使用从Ffowcs Williams-Hawkings方程导出的Farassat 1A计算声音并与测量结果进行比较。此外,通过更改其几何参数(如跨度,弦长和扭转角)对风扇进行了降噪修改。 /值比较和讨论了针对不同改装任务的空气动力学和声学变化趋势。对于螺旋桨的降噪可以得出一些有意义的结论。

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