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Reynolds Stress Models

The Reynolds stress model (RSM) determines the turbulent stresses by solving a transport equation for each stress component.

The RSM accounts for the effects of flow history and streamline curvature, as well as system rotation and stratification (Wilcox, 2000). Reynolds stress models are known to give superior results over one and two equation models when dealing with flows with streamline curvature, flows with sudden change in strain rate, and flows with secondary motions, all at the cost of an increased computing time (Bradshaw, 1997). There are many types of Reynolds stress models, the two most common being the RSM based on the dissipation rate (ε) and the RSM based on the eddy frequency (ω). In this section the dissipation rate (ε) model is discussed.

Transport Equations

Reynolds Stresses ¯ u'iu'j (1)
(ρ¯ u'iu'j)t+(ρ¯uk¯ u'iu'j)xk =PR+DR+Πij+DRM+DRT
Turbulent Dissipation Rate ε(2)
(ρε)t+(ρ¯ujε)xj =xj[(μ+μtσε)εxj]+Pε+Dε

Production Modeling

Reynolds Stresses ¯ u'iu'j (3)
PR=ρ(¯ u'iu'k¯ujxk+¯ u'ju'k¯uixk)
Turbulent Dissipation Rate ε (4)
Pε=Cε1εkμtS2=Cε1εkPk

Dissipation Modeling

Reynolds Stresses ¯ u'iu'j (5)
DR=2μ(¯uixk¯ujxk)
Turbulent Dissipation Rate ε (6)
Dε=Cε2ρε2k

Molecular Diffusion Modeling

Reynolds Stresses ¯ u'iu'j (7)
DRM=μxk(¯ u'iu'jxk)

Turbulent Diffusion Modeling

Reynolds Stresses ¯ u'iu'j (8)
DRT=μtρσkxk(¯ u'iu'jxk)

Pressure-Strain Modeling

Reynolds Stresses ¯ u'iu'j (9)
Πij=Πij,s+Πij,f+Πij,w

where Πij,s=C1ρεk(¯ u'iu'j23kδij) , Πij,f=Πij,f1+Πij,f2 , Πij,f1=C2(ρ(¯ uiuk¯ujxk+¯ ujuk¯uixk)xk(ρ¯uk¯ uiuj)) , Πij,f2=13δij(ρ(¯ ukuk¯ukxk+¯ ukuk¯ukxk)xk(ρ¯uk¯ ukuk)) , Πij,w=Πij,w1+Πij,w2 , Πij,w1=C3εncknc(¯ ukumηkηmδij32¯ uiukηjηk32¯ ujukηiηk)k3/2Cwεχ , Πij,w2=C4(Πkm,fηkηmδij32Πik,fηjηk32Πjk,fηiηk)k3/2Cwεχ

where ηk is the xk component of the unit normal to the wall and χ is the normal distance from the wall.

Modeling of Turbulent Viscosity μt

(10)
μt=ρCμk2ε

Model Coefficients

Cε1 = 1.44, Cε2 = 1.92, Cμ = 0.09, σk = 1.0, σε = 1.0, C1 = 1.8, C2 = 0.6, C3 = 0.5, C4 = 0.3, Cw = Cμ3/4κ