尾行边远场噪声和噪声源的特征在高入流流条件下
Laura Botero-Bolívar1, Fernanda L Dos Santos1, Cornelis H Venner1
1Engineering Fluid Dynamics, University of Twente, Enschede, Overijssel, 7522 NB, the Netherlands.
The Journal of the Acoustical Society of America
|February 1, 2024
概括
输入流显著增加机身噪声,特别是尾翼噪声,通过改变边界层和墙壁压力波动. 这项研究量化了不同气形和条件的噪声增加.
科学领域:
- 声学 声学 在声学方面
- 流体动力学 流体动力学
- 空气动力学 航空动力学
背景情况:
- 机身噪声在风能和航空等应用中是一个重要的限制.
- 输入流加剧了机身噪声,因为它影响了边界层和在气翼尾翼边缘附近的墙壁压力波动.
研究的目的:
- 为了研究流入流如何影响尾端噪声产生机制.
- 分析气翼几何学在流条件下的占主导地位的噪声源中的作用.
- 为了概括观察到的尾行边缘噪声的增加.
主要方法:
- 进行边界层和壁面压力波动在气翼尾翼边缘附近的测量.
- 在三个不同的气形上进行远场噪声测量.
- 分析流入流对墙壁压力频谱和跨度相关长度的影响.
主要成果:
- 输入流增加了墙壁压力频谱和跨度相关长度.
- 由于流入流,所有测试的气形和频率的尾行边缘噪声增加了2-15+dB.
- 尾行边缘噪声在较低的速度和较厚的气形上占主导地位.
结论:
- 输入流是增加机身噪声的关键驱动因素,特别是尾翼噪声.
- 气翼几何学和流入速度调节了前沿和后沿边缘噪声的贡献.
- 了解这些机制对于降低空气动力学应用中的噪声至关重要.
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