Abstract

Low-frequency narrow-band noise is one of the important components in the slat noise. Based on the transient flow field analysis for multi-element airfoil 30P-30N, the main mode characteristics of the slat pressure fluctuation are analyzed by means of proper orthogonal decomposition (POD) and dynamic model decomposition (DMD), and the key feature modes and the distribution of narrow-band frequencies for the slat are obtained. Empirical mode decomposition (EMD) and cross-correlation analysis are used to reconstruct the signal by preserving the low frequency characteristics of the original transient pressure signal. The locations of noise sources of the low-frequency narrow-band are determined according to the delay time and geometric relationship for characteristic points. The results show that the low-frequency narrow-band sound sources are mainly concentrated on regions of feature modes with large pressure fluctuations, such as slat trailing edge, downstream of the shear layer and the recirculation zone. Meanwhile, there are still some sound sources of low-frequency narrow-band distributed in regions of non-featured modes. The key characteristics of these regions are the interaction of flow structure between the trailing edge of the slat and the leading edge of the main wing due to collision of the shear layer.

Highlights

  • The analysis of noise features for multi⁃element airfoil based on slat configuration parameters[ J]

  • Based on the transient flow field analysis for multi⁃element airfoil 30P⁃30N, the main mode characteristics of the slat pressure fluctuation are analyzed by means of proper orthogonal decomposition ( POD) and dynamic model decomposition ( DMD), and the key feature modes and the distribution of narrow⁃band frequencies for the slat are obtained

  • Em⁃ pirical mode decomposition ( EMD) and cross⁃correlation analysis are used to reconstruct the signal by preserving the low frequency characteristics of the original transient pressure signal

Read more

Summary

Introduction

POD 与 DMD 压力模态云图是流场压力瞬态变 化特征的解构,在一定程度上反映了缝翼声源的分 布。 然而,必须注意到,流场压力脉动与声压传播是 有一定差别的;其原因就是有相当大的压力脉动能 量并没有辐射到远场。 为了进一步探索缝翼低频窄 带噪声源的分布特征,本文对原始瞬态压力脉动数 据进行处理,滤除高频和对低频窄带贡献较小的成 分,并利用相关性分析,探讨缝翼窄带噪声源的分布 特征。 2.3 低频窄带噪声源分布 号的相关系数 ρ ( imfi t) ( i 表示第 i 个 IMF 分量) ; 3) 的 IMF 分量和残差(rn) 累加获得新信号 x′(t) x′(t) = ∑ imfi(t) + rn ρi≥δ && Ai > 5 ( 12)

Results
Conclusion
Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call