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Acta Aeronautica et Astronautica Sinica ›› 2025, Vol. 46 ›› Issue (14): 331486.doi: 10.7527/S1000-6893.2025.31486

• Fluid Mechanics and Flight Mechanics • Previous Articles    

Experiment on acoustic impedance of large-thickness perforated plate

Chuanyang LIU1, Xiaoyu WANG1, Guangyu ZHANG1(), Xiaofeng SUN1,2   

  1. 1.Research Institute of Aero-Engine,Beihang University,Beijing 102206,China
    2.School of Energy and Power Engineering,Beihang University,Beijing 102206,China
  • Received:2024-11-04 Revised:2024-12-23 Accepted:2025-02-07 Online:2025-02-17 Published:1900-01-01
  • Contact: Guangyu ZHANG E-mail:guangyu.zhang@buaa.edu.cn
  • Supported by:
    Aero Engine and Gas Turbine Basic Science Center Project (P2022-B-Ⅱ-013-001);National Natural Science Foundation of China(52476024);Taihang Laboratory Funding Project (A2053)

Abstract:

Over-the-rotor liner and soft vans have received much attention as new noise reduction means, and large-thickness perforated plate is a feasible structural form for realizing these two noise reduction means. Therefore, the acoustic impedance characteristics of large-thickness perforated plates are investigated. Based on the impedance tube and flow tube test platforms, the acoustic impedance characteristics of large-thickness perforated plates are experimentally investigated in the absence and presence of grazing flow, and the applicability of the Beihang model to the prediction of acoustic impedance for large thickness perforated plates is explored. Under no grazing flow conditions, the test acoustic impedance of a solid perforated plate with a thickness of 8 mm shows good linear characteristics, and the Beihang model is able to accurately predict the acoustic impedance of the large-thickness perforated plate. Meanwhile, a honeycomb-cavity sandwich perforated plate structure is proposed for the case where the static blade has a hollow structure. Measurement results show that the acoustic impedance of this structure is mainly provided by the perforated plates on both sides, while the honeycomb-cavity in the middle provides only a small portion of the acoustic impedance. Under grazing flow conditions, the applicability of the Beihang model to the prediction of acoustic impedance for large-thickness perforated plates is investigated in terms of both acoustic impedance prediction accuracy and transmission loss. When the grazing flow velocities are 10 m/s and 20 m/s, the Beihang model can still accurately predict the acoustic impedance of large-thickness perforated plates. As the grazing flow velocity increases, the effect of plate thickness on vortex shedding in small holes begins to become apparent. When the grazing flow velocities reach 40 m/s and 60 m/s, the prediction error of the Beihang model based on the fitting of vortex shedding strength of the thin plate on the acoustic impedance of the large-thickness perforated plate starts to increase. However, in terms of the transmission loss, the transmission loss curves predicted by the Beihang model show a similar trend with that of the experimentally measured transmission loss curve. It can be seen that the Beihang model still provides valuable guiding for the engineering application of large-thickness perforated plates.

Key words: perforated plate, acoustic impedance, acoustic impedance tube, acoustic flow tube, transmission loss

CLC Number: