Abstract
AbstractAn improved approach for constrained large-eddy simulations (CLES) of wall-bounded compressible transitional flows is proposed by introducing an intermittency factor. The improved model is tested and validated with compressible channel flows at various Mach numbers and Reynolds numbers that are transitioning from laminar to turbulent states. The improved model is compared against traditional dynamic Smagorinsky model (DSM) and Direct Numerical Simulations (DNS), where the improved model is in better agreement with DNS results than traditional DSM model, in terms of mean velocity profiles, total Reynolds stress and total heat flux. Therefore, the proposed method can be used to accurately predict the temporal laminar-turbulent transition process of compressible wall-bounded flows.
Funder
National Numerical Wind Tunnel Project of China
National Natural Science Foundation of China
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Aerospace Engineering,Modeling and Simulation,Renewable Energy, Sustainability and the Environment,Civil and Structural Engineering
Reference47 articles.
1. Zhong X, Wang X (2012) Direct numerical simulation on the receptivity, instability, and transition of hypersonic boundary layers. Ann Rev Fluid Mech 44(1):527–561
2. Li F, Xie SF, Bi ZX, Gong J, Chen X, Ji F et al (2014) Experimental study of several on aerodynamic problems on hypersonic vehicles. Mod Def Technol 42(5):1–7
3. Fu S, Wang L (2013) RANS modeling of high-speed aerodynamic flow transition with consideration of stability theory. Prog Aerosp Sci 58:36–59
4. Orszag SA, Kells LC (1980) Transition to turbulence in plane Poiseuille and plane Couette flow. J Fluid Mech 96(1):159–205
5. Sayadi T, Hamman CW, Moin P (2013) Direct numerical simulation of complete H-type and K-type transitions with implications for the dynamics of turbulent boundary layers. J Fluid Mech 724:480–509
Cited by
1 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献