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k-epsilon and k-omega SST models

Short answer

Standard k-ε solves transport for k and ε, uses wall functions, and is robust for fully turbulent flows but poor in separation. SST k-ω blends k-ω near-wall integration (y+≈1) with k-ε in the free stream, includes a shear-stress limiter, and captures adverse pressure gradients and separation much better.

Explain the standard k-ε\varepsilon and the k-ω\omega SST turbulence models. Differentiate between them with respect to equations, near-wall treatment, strengths and limitations.

Both are two-equation eddy viscosity models: two transport equations give a velocity scale and a length (or time) scale, from which the eddy viscosity μt\mu_t is found (Boussinesq hypothesis).

Standard k-ε\varepsilon (Launder-Spalding)

Solves transport equations for turbulent kinetic energy kk and its dissipation rate ε\varepsilon:

μt=ρCμk2ε,Cμ=0.09\mu_t=\rho C_\mu\frac{k^2}{\varepsilon},\quad C_\mu=0.09 D(ρk)Dt=∇⋅[(μ+μtσk)∇k]+Pk−ρε\frac{D(\rho k)}{Dt}=\nabla\cdot\left[\left(\mu+\frac{\mu_t}{\sigma_k}\right)\nabla k\right]+P_k-\rho\varepsilon D(ρε)Dt=∇⋅[(μ+μtσε)∇ε]+C1εεkPk−C2ερε2k\frac{D(\rho\varepsilon)}{Dt}=\nabla\cdot\left[\left(\mu+\frac{\mu_t}{\sigma_\varepsilon}\right)\nabla\varepsilon\right]+C_{1\varepsilon}\frac\varepsilon kP_k-C_{2\varepsilon}\rho\frac{\varepsilon^2}{k}

with C1ε=1.44, C2ε=1.92, σk=1.0, σε=1.3C_{1\varepsilon}=1.44,\ C_{2\varepsilon}=1.92,\ \sigma_k=1.0,\ \sigma_\varepsilon=1.3. Valid for fully turbulent flow, so it uses wall functions near walls.

k-ω\omega SST (Menter)

A hybrid: the Wilcox k-ω\omega model near walls, which is switched by blending functions F1,F2F_1,F_2 to a transformed k-ε\varepsilon model in the free stream. Uses ω=ε/(Cμk)\omega=\varepsilon/(C_\mu k) (specific dissipation rate) and limits the shear stress in adverse pressure gradients through

μt=ρa1kmax⁡(a1ω, SF2)\mu_t=\frac{\rho a_1k}{\max(a_1\omega,\ SF_2)}

(the "shear stress transport" limiter, a1=0.31a_1=0.31).

Comparison

PointStandard k-ε\varepsilonk-ω\omega SST
Variablesk, εk,\ \varepsilonk, ωk,\ \omega
Near wallNeeds wall functions (y+y^+ 30-300)Integrates to the wall (y+≈1y^+\approx1); also works with wall functions
Adverse pressure gradient, separationPoor; delays separationGood; shear stress limiter
Free-stream sensitivityLowLow (due to blending)
Cost and robustnessRobust, cheap, widely usedSlightly costlier, more mesh needed at the wall
Best forFully turbulent internal flow, mixing, jets, industrial flowsExternal aerodynamics, boundary layers, turbomachinery, heat transfer
LimitationsOver-predicts k in stagnation regions; poor for swirl, strong curvature, low-ReReNeeds fine near-wall mesh; still isotropic eddy viscosity

Neither model captures anisotropy or strong swirl well; for those, RSM or LES is preferred.

✓ Answer checked by Claude Opus 5.5 (high effort)

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