[1] |
张涵信. 关于非定常流动的计算问题[C]//第六届全国流体力学会议论文集,2001. ZHANG H X. On the calculation of unsteady flow[C]//Papers of the Sixth National Conference on Fluid Dynamics, 2001(in Chinese).
|
[2] |
张涵信,周恒. 流体力学的基础研究[C]//第六届全国流体力学会议论文集,2001. ZHANG H X, ZHOU H. Basic research of fluid dynamics[C]//Papers of the Sixth National Conference on Fluid Dynamics, 2001(in Chinese).
|
[3] |
周恒. 新世纪对流体力学提出的要求[J]. 自然科学进展,2000,10(6):491-494. ZHOU H. Requirements for hydrodynamics in the new century[J]. Progress in Natural Science, 2000,10(6):491-494(in Chinese).
|
[4] |
SPALART P R, JOU W H. Comments on the feasibility of LES for wings and on the hybrid RANS/LES approach[C]//Advances in DNS/LES, 1st AFOSR International Conference on DNS/LES, 1997.
|
[5] |
徐晶磊,高歌,杨焱. 基于当地流动结构的RANS/LES混合模型[J]. 航空学报,2014,35(11):2992-2999. XU J L,GAO G,YANG Y. A RANS/LES hybrid model based on local flow structure[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(11):2992-2999(in Chinese).
|
[6] |
MORTON S. High Reynolds number DES simulations of vortex breakdown over a 70 degree delta wing[C]//21st Applied Aerodynamics Conference. Reston:AIAA, 2003.
|
[7] |
ALLEN R, MENDONCA F. RANS and DES turbulence model predictions of noise on the M219 cavity at M=0.85[J]. International Journal of Aeroacoustics, 2005, 4:135-151.
|
[8] |
TRAPIER S, DECK S. Delayed detached-eddy simulation and analysis of supersonic inlet buzz[J]. AIAA Journal, 2008, 46(1):118-131.
|
[9] |
FORSYTHE J R, SQUIRES K D. Detached-eddy simulation of the F-15E at high alpha[J]. Journal of Aircraft, 2004, 41(2):193-200.
|
[10] |
GRESCHNER B, THIELE F. Prediction of sound generated by a rod-airfoil configuration using EASM DES and the generalised Lighthill/FW-H analogy[C]//12th AIAA/CEAS Aeroacoustics Conference. Reston:AIAA, 2006.
|
[11] |
MENTER F R, KUNTZ M. Adaptation of eddy-viscosity turbulence models to unsteady separated flow behind vehicles[C]//Symposium on the Aerodynamics of Heavy Vehicles:Trucks, Buses and Trains, 2002.
|
[12] |
SPALART P R, DECK S. A new version of detached-eddy simulation, resistant to ambiguous grid densities[J]. Theoretical & Computational Fluid Dynamics, 2006, 20(3):181-195.
|
[13] |
SHUR M L, SPALART P R. A hybrid RANS-LES approach with delayed-DES and wall-modelled LES capabilities[J]. International Journal of Heat and Fluid Flow, 2008, 29(6):1638-1649.
|
[14] |
NIKITIN N V, NICOUD F. An approach to wall modeling in large-eddy simulations[J]. Physics of Fluids, 2000, 12(7):1629.
|
[15] |
袁先旭,邓小兵,谢昱飞,等. 超声速湍流流场的RANS/LES混合计算方法研究[J]. 空气动力学学报,2009, 27(6):723-728. YUAN X X, DENG X B, XIE Y F, et al. Research on the RANS/LES hybrid method for supersonic-hypersonic turbulence flow[J]. Acta Aerodynamica Sinica, 2009, 27(6):723-728(in Chinese).
|
[16] |
KAWAI S, FUJⅡ K. Compact scheme with filtering for large-eddy simulation of transional boundary layer[J]. AIAA Journal, 2008, 46(3):690-700.
|
[17] |
陈琦,司芳芳,陈坚强,等. RANS/LES在超声速突起物绕流中的应用研究[J]. 航空学报, 2013, 34(7):1531-1537. CHEN Q,SI F F,CHEN J Q,et al. Study of protuberances in supersonic flow with RANS/LES method[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(7):1531-1537(in Chinese).
|
[18] |
HERRIN J L, DUTTON J C. Base bleed experiments with a cylindrical afterbody in supersonic flow[J]. Journal of Spacecraft & Rockets, 1994,31(6):1021-1028.
|
[19] |
HAASE W, BRAZA M, REVELL A. DESider-A European effort on hybrid RANS-LES modelling[J]. Notes on Numerical Fluid Mechanics & Multidisciplinary Design, 2009, 103:341-346.
|
[20] |
袁先旭. 非定常流动数值模拟及飞行器动态特性分析研究[D]. 绵阳:中国空气动力研究与发展中心,2002. YUAN X X. Numerical simulation of unsteady flow and analysis of dynamic characteristics of aircraft[D]. Mianyang:China Aerodynamic Research and Development Center, 2002(in Chinese).
|
[21] |
VISBAL M R, SHANG J J S. Numerical investigation of the flow structure around a rapidly pitching airfoil:AIAA-1987-1424[R]. Reston:AIAA, 1987.
|
[22] |
RUMSEY C L, ANDERSON W K. Some numerical and physical aspects of unsteady Navier-Stokes computations over airfoils using dynamic meshes:AIAA-1988-0329[R]. Reston:AIAA, 1988.
|
[23] |
NIU Y Y, LIOU M S. Numerical simulation of dynamic stall using upwind methods with dual time stepping:AIAA-1997-1000[R]. Reston:AIAA, 1997.
|
[24] |
LANDON R H. NACA0012, oscillatory and transient pitching:AGARD-R-702[R]. 2000.
|
[25] |
PIZIALI R A. 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall:NASA TM-4632[R]. Washington, D.C.:NASA, 1994.
|
[26] |
XIAO Z Z, LIU J. Numerical dissipation effects on massive separation around tandem cylinders[J]. AIAA Journal, 2012, 50(5):1119-1136.
|
[27] |
刘周,杨云军,周伟江,等. 使用RANS/LES混合方法模拟翼型大迎角动态非定常分离流动[C]//第十四届全国分离流、旋涡和流动控制会议论文集, 2013. LIU Z, YANG Y J, ZHOU W J, et al. Using RANS/LES hybrid method to simulate dynamic unsteady separated flow of airfoil at high angle of attack[C]//Proceedings of the 14th National Conference on Separated Flow, Vortex and Flow Control, 2013(in Chinese).
|