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	Modelling flow transition in a hypersonic boundary layer with Reynolds-averaged Navier-Stokes approach
	Liang, Wang ; Song, Fu
	2010-10-12 ; 2010-10-12
关键词	hypersonic boundary-layer transition turbulence model intermittency factor TURBULENCE PREDICTION ONSET Physics, Multidisciplinary
中文摘要	Based on Reynolds-averaged Navier-Stokes approach, a laminar-turbulence transition model is proposed in this study that takes into account the effects of different instability modes associated with the variations in Mach numbers of compressible boundary layer flows. The model is based on k-omega-gamma three-equation eddy-viscosity concept with k representing the fluctuating kinetic energy, omega the specific dissipation rate and the intermittency factor gamma. The particular features of the model are that: 1) k includes the non-turbulent, as well as turbulent fluctuations; 2) a transport equation for the intermittency factor gamma is proposed here with a source term set to trigger the transition onset; 3) through the introduction of a new length scale normal to wall, the present model employs the local variables only avoiding the use of the integral parameters, like the boundary layer thickness delta, which are often cost-ineffective with the modern CFD (Computational Fluid Dynamics) methods; 4) in the fully turbulent region, the model retreats to the well-known k-omega SST (Shear Stress Transport) model. This model is validated with a number of available experiments on boundary layer transitions including the incompressible, supersonic and hypersonic flows past flat plates, straight/flared cones at zero incidences, etc. It is demonstrated that the present model can be successfully applied to the engineering calculations of a variety of aerodynamic flow transition.
语种	英语 ; 英语
出版者	SCIENCE PRESS ; BEIJING ; 16 DONGHUANGCHENGGEN NORTH ST, BEIJING 100717, PEOPLES R CHINA
内容类型	期刊论文
源URL	[http://hdl.handle.net/123456789/78979]
专题	清华大学
推荐引用方式 GB/T 7714	Liang, Wang,Song, Fu. Modelling flow transition in a hypersonic boundary layer with Reynolds-averaged Navier-Stokes approach[J],2010, 2010.
APA	Liang, Wang,&Song, Fu.(2010).Modelling flow transition in a hypersonic boundary layer with Reynolds-averaged Navier-Stokes approach..
MLA	Liang, Wang,et al."Modelling flow transition in a hypersonic boundary layer with Reynolds-averaged Navier-Stokes approach".(2010).

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