Impedance Eduction Based on Microphone Measurements or Liners Under Grazing Flow Conditions

被引:15
|
作者
Busse-Gerstengarbe, Stefan [1 ]
Richter, Christoph
Thiele, Frank H. [1 ]
Lahiri, Claus [2 ]
Enghardt, Lars [2 ]
Roehle, Ingo [3 ]
Ferrante, Piergiorgio [4 ]
Scofano, Antonio
机构
[1] Tech Univ Berlin, Inst Fluid Mech & Engn Acoust, CFDCAA Grp, D-10623 Berlin, Germany
[2] German Aerosp Ctr, DLR, Inst Prop Technol, Engine Acoust Dept, D-10623 Berlin, Germany
[3] German Aerosp Ctr, DLR, Inst Prop Technol, Turbine Dept, D-10623 Berlin, Germany
[4] AleniaAermacchi SpA, Tech Dept, ITV TACU, I-21040 Venegono Superiore, VA, Italy
关键词
FINITE-DIFFERENCE SCHEMES; RUNGE-KUTTA SCHEMES; BOUNDARY-CONDITIONS; LOW-DISSIPATION; ATTENUATION; UNIFORM; SOUND;
D O I
10.2514/1.J051232
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper presents the results of insertion loss measurements and numerical impedance eduction of three different liner samples. An overview of the test rig and methodology is given, and preprocessed results in terms of reflection and transmission coefficients as well as the energy dissipation are discussed. These coefficients are calculated for discrete frequencies within the investigated frequency range. Subsequently, a numerical postprocessing is performed in the time domain, and the educed impedance function for each sample and flow Mach number is presented. This postprocessing in the time domain uses an impedance model based on the extended Helmholtz resonator with five free parameters. The parameters of the model are fitted via an optimization, which determines the whole frequency response in one optimization process. The comparison of measured and numerically evaluated energy coefficients proves the reliability of the tools for impedance evaluation under flow conditions. Finally, the impedance results or the different samples are discussed, including a comparative study with Aermacchi data of the National Aerospace Laboratory (The Netherlands) flow tube and Aermacchi impedance tube experiments.
引用
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页码:867 / 879
页数:13
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