Constitutive Relations

Constitutive relations describe the relation between the stress tensor and the mean strain rate that is used in the Boussinesq approximation.

By default, the Boussinesq approximation implies a linear constitutive relation. Non-linear constitutive relations account for anisotropy of turbulence by adding non-linear functions of the strain and vorticity tensors. For the SST (Menter) K-Omega model in Simcenter STAR-CCM+, quadratic and cubic constitutive relations are available. The cubic constitutive relation is derived from a Reynolds stress model and thus represents an Explicit Algebraic Reynolds Stress Model (EARSM):

Constitutive Relation Formulation
Quadratic [325]
Figure 1. EQUATION_DISPLAY
TRANS,NL=-2μt0.04645(OSSO)
(1241)
Cubic [322], [327]
Figure 2. EQUATION_DISPLAY
TRANS,NL=ρk[β3(W*W*13IIΩI)+β4(S*W*W*S*)+β6(S*W*W*+W*W*S*IIΩS*23IVI)]
(1242)

where:

S is the strain rate tensor given by Eqn. (1130) and S* is given by:
Figure 3. EQUATION_DISPLAY
S*=1β*ωS
(1243)

where β* is given in K-Omega Model—Model Coefficients.

W is the vorticity tensor given by Eqn. (1132), W* is given by:
Figure 4. EQUATION_DISPLAY
W*=1β*ωW
(1244)

and:

Figure 5. EQUATION_DISPLAY
O=W(SW)(SW)
(1245)
Figure 6. EQUATION_DISPLAY
IIΩ=W*:W*T
(1246)
Figure 7. EQUATION_DISPLAY
IV=S*W*W*
(1247)

For the momentum equation Eqn. (665), the stress tensor TRANS is defined as:

Figure 8. EQUATION_DISPLAY
TRANS=TRANS,L+TRANS,NL
(1248)

where TRANS,L is given by Eqn. (1147).

Relation for Turbulent Viscosity

When applying the linear or the quadratic constitutive relation, the turbulent viscosity for the SST (Menter) K-Omega model is given by Eqn. (1207). For the cubic constitutive relation, μt is computed as:

Figure 9. EQUATION_DISPLAY
μ t = C μ β * ρ k T
(1249)

The coefficient Cμ is obtained from:

Figure 10. EQUATION_DISPLAY
Cμ=12(β1+IIΩβ6)
(1250)

where β1 and β6 are Model Coefficients.

Model Coefficients

The coefficients βi are given by:

Figure 11. EQUATION_DISPLAY
β1=N(2N27IIΩ)Q
(1251)
Figure 12. EQUATION_DISPLAY
β3=12IVNQ
(1252)
Figure 13. EQUATION_DISPLAY
β4=2(N22IIΩ)Q
(1253)
Figure 14. EQUATION_DISPLAY
β6=6NQ
(1254)
Figure 15. EQUATION_DISPLAY
Q=56(N22IIΩ)(2N2IIΩ)
(1255)

where N is given by:

Figure 16. EQUATION_DISPLAY
N={A33+P1+P23+sign(P1P2)|P1P2|3for  P20A33+2P12P26cos[13cos-1(P1P12P2)]for  P2<0
(1256)

where:

Figure 17. EQUATION_DISPLAY
P1=A3(A3227+920IIS23IIΩ)
(1257)
Figure 18. EQUATION_DISPLAY
P2=P12(A329+910IIS23IIΩ)3
(1258)
Figure 19. EQUATION_DISPLAY
A3=95+942.2max(1+β1eqIIS,0)
(1259)
Figure 20. EQUATION_DISPLAY
β1eq=65(8120(8120)22IIΩ)
(1260)
Figure 21. EQUATION_DISPLAY
IIS=S*:S*T
(1261)