本文采用声类比法探讨了射流中小尺度湍流远场噪声特性.此声类比理论基于线化欧拉方程及声源互易原理,建立了关联声源和远场声压的伴随格林函数,适于声波折射现象及小尺度湍流噪声计算.声场的边界采用完全匹配层边界条件,有效地避免了声波产生数值反射.为减小频散及耗散误差,时空导数均采用高阶预测-校正格式离散控制方程.计算结果与前人的实验相一致.
参考文献
[1] | Tam CKW. .Jet noise: Since 1952[J].Theoretical and Computational Fluid Dynamics,1998(1/4):393-405. |
[2] | Tam C K W;Auriault L .Mean Flow Refraction Effects on Sound Radiated from a Localized Source in Jets[J].J.Fluid Mechanics,1999,370:149-174. |
[3] | Khavaran A;Bridges J;Freund J B .A Parametric Study of Fine-Scale Turbulence Mixing Noise[NASA/TM-2002-211696][R].,2002. |
[4] | Alpert B K.Hybrid Gauss-Trapezoidal Quadrature Rules[J].SIAM Journal of Scientific Computing,1999 |
[5] | Hagstrom T;Nazarov I .Absorbing Layers and Radiation Boundary Condition for Jet Flow Simulations[AIAA 2002-2606][R].,2002. |
[6] | Lush P A .Measurement of Subsonic Jet Noise and Comparison with Theory[J].Journal of Fluid Mechanics,1971,46:477-500. |
[7] | Stromberg J L;McLaughlin D K;Troutt T R .Flow Field and Acoustic Properties of Mach Number 0.9 Jet at a Low Reynolds Number[J].J.of Sound and Vib,1980,72:159-176. |
上一张
下一张
上一张
下一张
计量
- 下载量()
- 访问量()
文章评分
- 您的评分:
-
10%
-
20%
-
30%
-
40%
-
50%