Applications of scale-adaptive simulation technique based on one-equation turbulence model

被引:12
作者
Xu, Chang-yue [1 ]
Zhou, Tao [1 ]
Wang, Cong-lei [1 ]
Sun, Jian-hong [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Aerosp Engn, Nanjing 210016, Peoples R China
基金
中国国家自然科学基金;
关键词
turbulence; detached-eddy simulation; scale-adaptive simulation; cylinder; LARGE-EDDY SIMULATION; CIRCULAR-CYLINDER; FLOW;
D O I
10.1007/s10483-015-1898-9
中图分类号
O29 [应用数学];
学科分类号
070104 ;
摘要
A modified scale-adaptive simulation (SAS) technique based on the Spalart-Allmaras (SA) model is proposed. To clarify its capability in prediction of the complex turbulent flow, two typical cases are carried out, i.e., the subcritical flow past a circular cylinder and the transonic flow over a hemisphere cylinder. For comparison, the same cases are calculated by the detached-eddy simulation (DES), the delayed-detached eddy simulation (DDES), and the XY-SAS approaches. Some typical results including the mean pressure coefficient, velocity, and Reynolds stress profiles are obtained and compared with the experiments. Extensive calculations show that the proposed SAS technique can give better prediction of the massively separated flow and shock/turbulent-boundary-layer interaction than the DES and DDES methods. Furthermore, by the comparison of the XY-SAS model with the present SAS model, some improvements can be obtained.
引用
收藏
页码:121 / 130
页数:10
相关论文
共 20 条
[1]  
[Anonymous], 2005, 43 AIAA AER SCI M EX
[2]  
Breuer M, 1998, INT J NUMER METH FL, V28, P1281, DOI 10.1002/(SICI)1097-0363(19981215)28:9<1281::AID-FLD759>3.0.CO
[3]  
2-#
[4]   Numerical investigation of the compressible flow past an aerofoil [J].
Chen, Li-Wei ;
Xu, Chang-Yue ;
Lu, Xi-Yun .
JOURNAL OF FLUID MECHANICS, 2010, 643 :97-126
[5]  
Eckelmann H, 1993, BLUFF BODY WAKE DYNA
[6]  
Gao Z. R., 2010, J BEIJING U AERONAUT, V36, P415
[7]   TRANSONIC VISCID-INVISCID FLOW INTERACTION ABOUT A HEMISPHERE-CYLINDER [J].
HSIEH, T .
AIAA JOURNAL, 1978, 16 (07) :651-655
[8]  
Menter F. R., 2003, 41 AER SCI M EXH 200
[9]  
Ong L, 1996, EXP FLUIDS, V20, P441, DOI 10.1007/BF00189383
[10]   Large-eddy simulation: achievements and challenges [J].
Piomelli, U .
PROGRESS IN AEROSPACE SCIENCES, 1999, 35 (04) :335-362