Acoustic Analogy Formulations Accelerated by Fast Multipole Method for Two-Dimensional Aeroacoustic Problems

被引:19
|
作者
Wolf, William R. [1 ]
Lele, Sanjiva K. [1 ]
机构
[1] Stanford Univ, Dept Aeronaut & Astronaut, Dept Mech Engn, Stanford, CA 94305 USA
关键词
SOUND GENERATION; ERROR ANALYSIS; EQUATIONS; SCATTERING; SIMULATION; CYLINDER; FLOW;
D O I
10.2514/1.J050338
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The calculation of acoustic field solutions due to aeroacoustic sources is performed for a large number of observer locations. Sound generation by vortex shedding is computed by a hybrid method and an accurate two-dimensional direct calculation, and the results are compared. The hybrid approach uses direct calculation for near-field source computations and the Ffowcs-Williams Hawkings equation as the acoustic analogy formulation. The integrations of surface dipole and volume quadrupole source terms appearing in the Flowcs-Williams Hawkings formulation are accelerated by a wideband multilevel adaptive fast multipole method. The wideband multilevel adaptive fast multipole method presented here applies a plane-wave expansion formulation for calculations in the high-frequency regime and a partial-wave expansion formulation in the low-frequency regime. The method is described in detail for the solution of a two-dimensional Green's function that incorporates convective effects. The method presented in this work is applied to two-dimensional calculations. However, it can be easily extended to three-dimensional calculations of surface monopole and dipole source terms and volume quadrupole source terms. Results for acoustic field solutions obtained by the accelerated Howes-Williams Hawkings formulation are 2 orders of magnitude faster when compared with the direct computation of the Howes-Williams Hawkings equation.
引用
收藏
页码:2274 / 2285
页数:12
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