Numerical Investigation on the Aerodynamic and Aeroacoustic Characteristics in New Energy Vehicle Cooling Fan with Shroud

被引:2
|
作者
Huang, Baoding [1 ]
Xu, Jinqiu [2 ]
Wang, Jingxin [2 ]
Xu, Linjie [2 ]
Chen, Xiaoping [1 ]
机构
[1] Zhejiang Sci Tech Univ, Key Lab Fluid Transmiss Technol Zhejiang Prov, Hangzhou 310018, Peoples R China
[2] Zhejiang Yinlun Machinery Co Ltd, Key Lab Smart Thermal Management Sci & Technol Veh, Taizhou 317200, Peoples R China
基金
中国国家自然科学基金;
关键词
cooling fan; shroud; large eddy simulation; pressure fluctuation; sound pressure level; NARROW-BAND; NOISE; FLOW;
D O I
10.3390/pr12020333
中图分类号
TQ [化学工业];
学科分类号
0817 ;
摘要
The cooling fan is one of the important noise sources for new energy vehicles, and the research on its aerodynamic and aeroacoustic characteristics is of great help to improve the noise, vibration and harshness performance of new energy vehicles. However, most of these studies focus on the impeller, and little consideration has been given to the study of the shroud. Based on the coupling calculation method of large eddy simulation and the Ffowcs-Williams and Hawkings acoustics model, the aerodynamic and aeroacoustic characteristics in a cooling fan with the shroud are investigated at flow rates from 0.623 kg/s to 1.019 kg/s (where 0.865 kg/s is the flow rate corresponding to the best efficiency point). The accuracy of numerical simulation results is verified by the grid independence verification and the comparison of experimental data. Research shows that several large-scale vortex structures are observed in the clearance between the impeller and the shroud. The maximum peak-to-peak values of pressure fluctuation at different flow rates occur in the intermediate section or outlet section of the shroud. Although the shroud contributes relatively less to the far field noise, its different distribution may change the position of the maximum sound pressure level. The dominant frequency of pressure fluctuation equals the blade passage frequency (BPF) and the maximum SPL is around the BPF, both of which are independent of flow rates. The maximum SPL and the amplitude of the dominant frequency decrease as the flow rate increases.
引用
收藏
页数:17
相关论文
共 50 条
  • [31] Numerical and experimental investigations on the aerodynamic and aeroacoustic performance of the blade winglet tip shape of the axial-flow fan
    Ryu, Seo-Yoon
    Cheong, Cheolung
    Kim, Jong Wook
    Park, Byeong Il
    JOURNAL OF THE ACOUSTICAL SOCIETY OF KOREA, 2024, 43 (01): : 103 - 111
  • [32] AERODYNAMIC AND AEROTHERMAL INVESTIGATION OF THE FLOW AROUND AN HPT ROTOR SHROUD: HEAT TRANSFER AND COOLING EFFECTIVENESS
    Lehmann, Knut
    Kanjirakkad, Vasudevan
    Hodson, Howard
    PROCEEDINGS OF THE ASME TURBO EXPO 2011, VOL 5, PTS A AND B, 2012, : 1375 - 1384
  • [33] Numerical simulation of vehicle aerodynamic characteristics based on DRSM
    State Key Laboratory of Automobile Dynamic Simulation, Jilin University, Changchun 130022, China
    不详
    不详
    Jilin Daxue Xuebao (Gongxueban), 2008, 3 (504-507):
  • [34] Numerical and Experimental Investigation of Aerodynamic Performance for a Straight Turbine Cascade With a Novel Partial Shroud
    Liu, Yan
    Zhang, Tian-Long
    Zhang, Min
    Zhang, Meng-Chao
    JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2016, 138 (03):
  • [35] Numerical Investigation on Aerodynamic and Thermal Characteristics of Hydrodynamic Foil Thrust Bearing with a Radial Cooling Inflow
    Gao Q.-H.
    Zhang J.-Z.
    Sun W.-J.
    Zhang J.-Y.
    Tuijin Jishu/Journal of Propulsion Technology, 2022, 43 (11):
  • [36] Numerical Investigation on Aerodynamic and Heat Transfer Characteristics of Sweeping Impingement and Film Composite Cooling Structure
    Kong X.-C.
    Zhang Z.-Q.
    Li G.-Q.
    Zhu J.-Q.
    Xu J.-L.
    Zhang Y.-F.
    Tuijin Jishu/Journal of Propulsion Technology, 2022, 43 (10):
  • [37] Aerodynamic design and numerical investigation of a highly loaded meridian acceleration fan
    Jin, Hai-Liang
    Jin, Dong-Hai
    Peng, Ze-Yan
    Gui, Xing-Min
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2011, 26 (07): : 1638 - 1646
  • [38] A numerical investigation into the aerodynamic effect of pressure pulses on a tunnel ventilation fan
    Cardillo, Lucio
    Corsini, Alessandro
    Delibra, Giovanni
    Rispoli, Franco
    Sheard, Anthony G.
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2014, 228 (03) : 285 - 299
  • [39] Numerical investigation of geometric parameter effects on the aerodynamic performance of a Bladeless fan
    Jafari, Mohammad
    Afshin, Hossein
    Farhanieh, Bijan
    Sojoudi, Atta
    ALEXANDRIA ENGINEERING JOURNAL, 2016, 55 (01) : 223 - 233
  • [40] Experimental and numerical investigation on aerodynamic performance of a highly loaded fan stator
    Tao, Li-Quan
    Sun, Peng
    Yang, Kun
    Pan, Ruo-Chi
    Tuijin Jishu/Journal of Propulsion Technology, 2015, 36 (09): : 1331 - 1338