论文标题
前沿锯齿对使用新型CFD信息分析的混合流风扇的声学特征的形态学影响
Morphological effects of leading-edge serrations on the acoustic signatures of mixed flow fan analyzed using novel CFD-informed methods
论文作者
论文摘要
前沿(LE)噪声是宽带噪声的常见来源,可以使用附加的LE锯齿来抑制宽带噪声。我们对使用实验,计算流体动力学(CFD)和FFOWCS Williams-Hawkings(FWH)进行了类似的猫头鹰启发的LE锯齿的间隔,长度和倾斜角度的形态效应进行了综合研究。基于使用大型模拟的FWH类比开发了一种新型的表面噪声强度(SNS)可视化方法,并提出了CFD信息的指数SAPG来评估使用压力梯度的流动分离的严重程度,该梯度可有效地检查声学源和分离。声学测量表明,在各种形态下,锯齿的强大权衡解决能力,SNS可视化表明分离引起的LE噪声被大大抑制。三分之一的八度分析表明,与在100-3k Hz上缩小间隔相比,延长锯齿长度可以更有效地降低分离噪声。较小的间隔是更可取的,而最佳长度与音调噪声相关。此外,小倾斜角(低于20度)使迎面而来的流量减速,从而减轻了降落,因此可以通过缓冲效应进一步抑制LE噪声。较重的倾斜角(超过40度)会引起额外的尖端涡流,从而导致高碳的湍流障碍噪声,并在超过4K Hz的频率下宽带噪声急剧增加。因此,我们的研究阐明了LE锯齿对旋转装置的气声特征的形态学作用,同时为声学分析提供了有用的方法。
Leading-edge (LE) noise is a common source of broadband noise for fans that can be suppressed using appended LE serrations. We conduct an integrated study of the morphological effects of interval, length, and inclination angle of owl-inspired LE serrations on the aeroacoustic characteristics of a mixed flow fan using experiments, computational fluid dynamics (CFD), and the Ffowcs Williams-Hawkings (FWH) analogy. A novel method for surface noise strength (SNS) visualization was developed based on the FWH analogy with large-eddy simulations, and a CFD-informed index SAPG is proposed to evaluate the severity of flow separation with pressure gradient, which are verified to be effective in examining the acoustic sources and chordwise separation. Acoustic measurements show the robust tradeoff solving capability of the serrations under various morphologies and the SNS visualizations indicate that the separation-induced LE noise is suppressed considerably. One-third octave analyses suggest that extending serration length can lower separation noise more effectively than shrinking the interval over 100-3k Hz. A smaller interval is more desirable while an optimal length exists in association with tonal noise. Moreover, small inclination angles (below 20 degrees) enable the deceleration of oncoming flows with stagnation relieved, and consequently, further suppress the LE noise, by a flow-buffering effect. Heavy inclination angles (over 40 degrees) induce an additional tip vortex, causing high-coherence turbulence impingement noise and resulting in a drastic increase in broadband noise at frequencies exceeding 4k Hz. Our study thus clarifies the morphological effects of LE serrations on aeroacoustic signatures of rotary devices while providing useful methods for acoustic analyses.