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考 虑 剪 切 流 的 航 空 声 衬 三 维 阻 抗 直 接 提 取 方 法

Translated title of the contribution: A three-dimensional straightforward method for acoustic liner impedance eduction under shear grazing flow
  • Lingfeng Chen
  • , Yunxiao Han
  • , Boyu Feng
  • , Zhiliang Hong*
  • , Xiaoyu Wang
  • , Lin Du
  • *Corresponding author for this work
  • Civil Aviation University of China

Research output: Contribution to journalArticlepeer-review

Abstract

The development of broadband acoustic liners requires taking the three-dimensional acoustic field into con⁃ sideration in impedance eduction. However,in existing three-dimensional impedance eduction methods,the grazing flow is generally assumed to be uniform,which is inconsistent with the actual situation of shear flow in flow ducts. To simultaneously solve the problems of three-dimensional acoustic field and shear grazing flow in acoustic liner imped⁃ ance eduction,a three-dimensional straightforward method considering a one-dimensional equivalent shear flow is de⁃ veloped. Using sound pressure data from a rectangular array of measuring points arranged on the rigid wall opposite to the liner surface,spanwise modal decomposition is firstly conducted to obtain intermediate variables,which can then be solved through Runge-Kutta iteration to compute the axial wavenumber. Finally,impedance is educed accord⁃ ing to the impedance boundary conditions. The accuracy of this method is verified through numerical simulation experi⁃ ments based on the finite element method for both plane-wave and plane-wave dominant incidence. By comparing the educed impedances with and without considering the shear grazing flow,it can be found that although shear flow has a relatively small impact on impedance eduction in the mid to low frequency range below the cutoff frequency,it may significantly affect the accuracy of the eduction result in the high frequency range. Moreover,as the flow Mach number increases,the influence of shear flow becomes more important.

Translated title of the contributionA three-dimensional straightforward method for acoustic liner impedance eduction under shear grazing flow
Original languageChinese (Traditional)
Article number630333
JournalHangkong Xuebao/Acta Aeronautica et Astronautica Sinica
Volume45
Issue number23
DOIs
StatePublished - 15 Dec 2024

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