流速和仰角对 NACA 0012 翼面气动噪声的影响

Hussein K. Mohammad, Bade Shrestha, V. Kilchyk
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引用次数: 0

摘要

风能是当今市场上主要的可再生能源之一。本研究调查了风速和攻角对气动噪声的影响。使用了四种不同的机翼样本。采用了三种风速(5、10、15 米/秒)。结果表明,气动噪声与流速直接相关。数据显示,当流速增加(5 m/s)时,噪声平均增大(10 dB)。随着流速的增加,速度剪切力也随之增加,最终导致气动噪声增大。至于攻角,它对气动噪声也有影响。结果显示,当攻角从(5 度)增加到(10 度)时,整体声压级增加了(1-4 分贝),而当攻角从(10 度)增加到(15 度)时,整体声压级增加了(1-6 分贝)。这项研究是在亚音速流动条件和雷诺数(3.3×104)下进行的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The effect of Flow Speed and Angle of Attack on the Aerodynamic Noise of NACA 0012 Airfoil
Wind energy is one of the main sources of renewable energy in the market today. The influence of the wind speed and the angle of attack on the aerodynamic noise was investigated in this study. Four different samples of airfoils were used. Three speeds (5, 10, 15 m/s) were employed. The results revealed that the aerodynamic noise was associated directly with the flow speed. The data showed that when the velocity increases by (5 m/s), the noise gets louder by an average amount of (10 dB). As the increase of flow velocity increased the velocity shear, this eventually increased the aerodynamic noise. As for the angle of attack, it had an effect on the aerodynamic noise as well. The results showed an increase in the overall sound pressure level between (1-4 dBA) when the angle of attack increased from (5 degrees) to (10 degrees), while there was an increase (1-6 dBA) when the angle of attack increased from (10 degrees) to (15 degrees). This study was conducted under subsonic flow condition and Reynolds number (3.3×104).
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