将分离涡模拟方法应用于高雷诺数压气机静叶有大分离的复杂流动计算中,研究该方法对分离的模拟能力.采用约280万网格,SA计算仅能得到定常结果.DES计算在叶片中部小分离区域,所得到的非定常波动较弱,尾迹掺混略慢于SA,结果整体上与SA类似.在叶片端壁附近有大分离的区域,DES结果捕捉到了明显的非定常现象与压力波动,计算表明吸力面涡脱落会加强掺混,而端壁分离则会加强尾迹.另外,DES计算比SA更详细地描述了涡结构.这表明DES有比SA更好的模拟大分离的能力.计算结果也加深了对静叶角涡与尾迹发展的认识.
参考文献
[1] | Raverdy B;Mary I;Sagaut P .High-Resolution Large-Eddy Simulation of Flow Around Low-Pressure Turbine Blade[J].AIAA Journal,2003,41(03):390-397. |
[2] | 李雪松,徐建中.低压高负荷涡轮叶栅的大涡模拟[J].工程热物理学报,2007(03):403-405. |
[3] | S. Sarkar;Peter R. Voke .Large-Eddy Simulation of Unsteady Surface Pressure Over a Low-Pressure Turbine Blade due to Interactions of Passing Wakes and Inflexional Boundary Layer[J].Journal of turbomachinery,2006(2):221-231. |
[4] | Spalart P R;Jou W H;Strelets M.Comments on the Feasibility of LES for Wings,and on a Hybrid RANS/LES Approach.Advance in DNS/LES[A].Greyden Press,Columbus,OH,1997 |
[5] | Aroon K. Viswanathan;Danesh K. Tafti .Detached Eddy Simulation of Turbulent Flow and Heat Transfer in a Ribbed Duct[J].Journal of Fluids Engineering: Transactions of the ASME,2005(5):888-896. |
[6] | 李雪松,顾春伟,徐建中.新型高低速流统一算法及其叶轮机应用[J].航空学报,2007(06):1334-1338. |
[7] | Li X S;GU C W;Xu J Z.Research of Preconditioned Roe Scheme for All Speed Flows in Turbomachinery[A].,2007 |
[8] | 李雪松,徐建中.一种非定常N-S方程并行求解设计[J].工程热物理学报,2008(01):52-54. |
[9] | Spalart PR;Deck S;Shur ML;Squires KD;Strelets MK;Travin A .A new version of detached-eddy simulation, resistant to ambiguous grid densities[J].Theoretical and Computational Fluid Dynamics,2006(3):181-195. |
[10] | Jeong J.;Hussain F. .ON THE IDENTIFICATION OF A VORTEX[J].Journal of Fluid Mechanics,1995(0):69-94. |
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%