Time-domain numerical simulation of a flow-impedance tube

被引:74
|
作者
Ozyoruk, Y [1 ]
Long, LN
Jones, MG
机构
[1] Middle E Tech Univ, Dept Aeronaut Engn, TR-06531 Ankara, Turkey
[2] Penn State Univ, Dept Aerosp Engn, University Pk, PA 16802 USA
[3] NASA, Langley Res Ctr, Lockheed Martin Engn & Sci Serv, Hampton, VA 23681 USA
关键词
flow-impedance tube; computational aeroacoustics; impedance conditions; z-transforms; nonreflecting boundary conditions; finite difference;
D O I
10.1006/jcph.1998.5919
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
An efficient method has been developed for. the application of the surface acoustic impedance condition in time-domain solutions of aeroacoustic problems, such as the broadband-frequency simulation of a flow-impedance tube, The basis for this method is the standard impedance condition stated in the frequency domain as the particle displacement continuity equation. The development of the time-domain impedance condition follows the relations among the frequency. z-, and discrete-time domains and a rational function representation of the impedance in the z-domain. The resultant impedance condition consists of finite, infinite-impulse-response type, digital filter operations in the time domain, which is very suitable to computational aeroacoustics algorithms. This paper describes the present approach and discusses the time-domain numerical simulations of the NASA Langley how-impedance tube with a constant depth ceramic tubular liner. Both single and broadband-frequency simulations are performed. Excellent agreement is shown with experimental data at various frequencies and flow conditions. (C) 1998 Academic Press.
引用
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页码:29 / 57
页数:29
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