Enhancing Axial Fan Noise Reduction through Innovative Wavy Blade Configurations

Document Type : Regular Article

Authors

School of Energy and Power Engineering, Xi’an Jiaotong University, Shaanxi, 710049, China

Abstract

Noise is one of the key indicators to evaluate axial flow fans, and in many cases, it is also the only indicator for determining their suitability for use. In this study, a new method to reduce axial fan’s noise was proposed for changing the section chord length to transform the blades of two axial fans with the same design parameters but distinct chord lengths to wavy blades. The aerodynamic calculations and noise reduction mechanism of the wavy configuration of the two fans were studied by combining CFD of large eddy simulation with the Lighthill acoustic analogy method. The results showed that the main mechanism contributing to noise reduction through wavy configuration was the promotion of transformation of the blade surface's layered vortex structure into an uncorrelated comb vortex structure. For fan blades with smaller chord lengths, the comb structure with low spanwise correlation was still maintained after the trailing edge, while for fan blades with larger chord lengths, the comb structure of the shedding vortex rapidly dissipated downstream of the trailing edge. Under the rated design conditions, the implementation of wavy leading edge blades resulted in noise reductions of 1.9 dB and 1.5 dB for the two fans, respectively, while wavy trailing edge blades yielded reductions of 2.6 dB and 2.1 dB, respectively. Furthermore, the adoption of wavy configuration induced a phenomenon of pressure increase and efficiency decrease in both axial fans at medium and low flow rates, with minimal impact at high flow rates. These outcomes underscored the superior noise reduction efficacy of the wavy trailing edge blades, offering a promising way for the noise reduction design of axial flow fans.

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Cao, H., Zhang, M., Cai, C., & Zhang, Z. (2020). Flow topology and noise modeling of trailing edge serrations. Applied Acoustics, 168, 107423. https://doi.org/10.1016/j.apacoust.2020.107423
Castegnaro, S. (2018). Aerodynamic design of low-speed axial-flow fans: a historical overview. Designs, 2(3). https://doi.org/10.3390/designs2030020
Cavalieri, A. V. G., Daviller, G., Comte, P., Jordan, P., Tadmor, G. & Gervais, Y. (2011). Using large eddy simulation to explore sound-source mechanisms in jets. Journal of Sound and Vibration, 330(17), 4098-4113. https://doi.org/10.1016/j.jsv.2011.04.018
Valencia, E., Hidalgo, V., Nalianda, D., Laskaridis, P., & Singh, R. (2017). Discretized miller approach to assess effects on boundary layer ingestion induced distortion. Chinese Journal of Aeronautics, 30(1), 235-248. https://doi.org/10.1016/j.cja.2016.12.005
Haeri, S., Kim, J. W., Narayanan, S., & Joseph, P. (2013). 3D calculations of aerofoil-turbulence interaction noise and the effect of wavy leading edges. AIAA/CEAS Aeroacoustics Conference. https://doi.org/10.2514/6.2014-2325
Hansen, K. L., Kelso, R. M., & Doolan, C. J. (2010). Reduction of flow induced tonal noise through leading edge tubercle modifications. AIAA/CEAS Aeroacoustics Conference. https://doi.org/10.2514/6.2010-3700
Hersh, A. S., Soderman, P. T., & Hayden, R. E. (1974). Investigation of acoustic effects of leading-edge serrations on airfoils. Journal of Aircraft, 11, 197-202. https://doi.org/10.2514/3.59219
Howe, M. S. (1991). Aerodynamic noise of a serrated trailing edge. Journal of Fluids and Structures, 5(1), 33-45. https://doi.org/10.1016/0889-9746(91)80010-B
Howe, M. S. (1998). Noise produced by a sawtooth trailing edge. Acoustical Society of America Journal, 90(1), 482-487. https://doi.org/10.1121/1.401273
Koca, K., Genc, M. S., Acikel, H. H., Cagdas, M., & Bodur, T. M. (2018). Identification of flow phenomena over NACA 4412 wind turbine airfoil at low reynolds numbers and role of laminar separation bubble on flow evolution. Energy, 144(FEB.1), 750-764. https://doi.org/10.1016/j.energy.2017.12.045
Krömer, F., Czwielong, F., & Becker, S. (2019). Experimental investigation of the sound emission of skewed axial fans with leading-edge serrations. AIAA Journal, 57(12), 5182-5196. https://doi.org/10.2514/1.J058134
Krömer, F., Renz, A., & Becker, S. (2018). Experimental Investigation of the Sound Reduction by Leading-Edge Serrations in Axial Fans. AIAA Journal, 56, 2086-2090. https://doi.org/10.2514/1.J056355
Lele, S. K., Mendez, S., Ryu, J., Nichols, J., Shoeybi, M., & Moin, P. (2010). Sources of high-speed jet noise: Analysis of LES data and modeling. Procedia Engineering, 6, 84-93. https://doi.org/10.1016/j.proeng.2010.09.010
Li, G. P., Ma, Z. L., Chen, C. S., Zhang, Y., Wang, Q., & Chen, E. Y. (2021). Experimental study on noise reduction characteristics of slanting serrated trailing edge blades. Journal of Physics: Conference Series, 1885, 042011. https://doi.org/10.1088/1742-6596/1885/4/042011
Lin, J. W., Liu, H. L., Dong, L., Zhou, R. Z., & Hua, R. N. (2022). Analysis of the sound field characteristics of a muffler at different flow conditions. Journal of Applied Fluid Mechanics, 16(1), 147-156. https://doi.org/10.47176/jafm.16.01.1295
Liu, J. M., Zhang, T., & Zhang, Y. O. (2013). Numerical study on flow-induced noise for a steam stop-valve using large eddy simulation. Journal of Marine Science & Application, 12(3), 351-360. https://doi.org/10.1007/s11804-013-1195-9
Nyquist, H. (1928). Certain topics in telegraph transmission theory. Transactions of the American Institute of Electrical Engineers, 47, 617-644. https://doi.org/10.1109/T-AIEE.1928.5055024
Rao, C., Ikeda, T., Nakata, T., & Liu, H. (2017). Owl-inspired leading-edge serrations play a crucial role in aerodynamic force production and sound suppression. Bioinspiration & Biomimetics, 12(4), 046008. https://doi.org/10.1088/1748-3190/aa7013
Sandboge, R., Caro, S., Ploumhans, P., Ambs, R., Schillemeit, B., Washburn, K., & Shakib, F. (2006). Validation of a CAA formulation based on lighthill's analogy using AcuSolve and ACTRAN/LA on an idealized automotive HVAC blower and on an axial fan. AIAA/CEAS Aeroacoustics Conference. https://doi.org/10.2514/6.2006-2692
Shur, M. L., Spalart, P. R., & Strelets, M. K. (2011). LES-based evaluation of a microjet noise reduction concept in static and flight conditions. Journal of Sound & Vibration, 330(17), 4083-4097. https://doi.org/10.1016/j.jsv.2011.02.013
Tan, J., Dong, P., Gao, J., Wang, C., & Zhang, L. (2023). Coupling bionic design and numerical simulation of the wavy leading-edge and seagull airfoil of axial flow blade for air-conditioner. Journal of Applied Fluid Mechanics, 16(7), 1316-1330. https://doi.org/10.47176/jafm.16.07.1634
Zhai, C., Tang, Z., Zou, Q., & Qin, L. (2016). Experimental study on the noise characteristics regarding axial auxiliary fans and the noise reduction performance of mufflers. Arabian Journal for Science & Engineering, 41(12), 1-10. https://doi.org/10.1007/s13369-016-2165-8
Zhang, C., Ji, L., Zhou, L., & Sun, S. (2020). Effect of blended blade tip and winglet on aerodynamic and aeroacoustic performances of a diagonal fan. Aerospace Science and Technology, 98, 105688. https://doi.org/10.1016/j.ast.2020.105688
Zhang, Y. O., Zhang, T., & Li, T. Y. (2014). Flow-induced noise simulation based on LES/Lighthill hybrid method. ICMECS, 428-431. https://doi.org/10.4028/www.scientific.net/AMM.614.428
Zhou, H., Wang, L., Huang, Z. F., & Ren, J. Z. (2022). Shedding vortex simulation method based on viscous compensation technology research. Chinese Physics B, 31(4). https://doi.org/10.1088/1674-1056/ac29ae
Zhou, S., Li, H., Wang, J., Wang, X., & Ye, J. (2014). Investigation acoustic effect of the convexity-preserving axial flow fan based on bezier function. Computers & Fluids, 102, 85-93. https://doi.org/10.1016/j.compfluid.2014.06.019
Zuo, Z. G., Huang, Q., & Liu, S. (2019). An analysis on the flow field structures and the aerodynamic noise of airfoils with serrated trailing edges based on embedded large eddy flow simulations. Journal of Applied Fluid Mechanics, 12(2), 327-339. https://doi.org/10.29252/jafm.12.02.29142