Morphological effects of leading-edge serrations on the acoustic signatures of mixed flow fan analyzed using novel CFD-informed methods

TL;DR

This study investigates how owl-inspired leading-edge serrations affect fan noise, using advanced CFD and experimental methods to optimize serration design for noise reduction.

Contribution

It introduces novel CFD-informed visualization and evaluation methods to analyze the morphological effects of serration parameters on fan noise.

Findings

Extending serration length reduces separation noise more effectively.

Small inclination angles (<20°) further suppress noise by flow buffering.

Large inclination angles (>40°) increase broadband noise due to vortex formation.

Abstract

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.