SpectraSim Documentation
Parameter · 06 Solver Settings

Turbulent kinetic energy relaxation

numerics.relaxation.k Step 06 · Solver Settings

Under-relaxation of the transport equation of the turbulent kinetic energy kk in the steady solver.

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Theory

The kk equation of the SST model (Turbulence model) is relaxed implicitly in the same way as momentum, equation (1): the diagonal is divided by αk\alpha_k and the old value is carried on the right-hand side, so the converged solution is unchanged. kk and ω\omega are strongly coupled through the eddy viscosity. Too little relaxation lets the eddy viscosity jump between iterations near the jets; too much slows the convergence of the whole system.

The auto values for every solver are in the table of Pressure relaxation.

Equations

aPαk kP=∑nbanbknb+b+1−αkαk aP kPold\frac{a_P}{\alpha_k}\,k_P = \sum_{nb} a_{nb}k_{nb} + b + \frac{1-\alpha_k}{\alpha_k}\,a_P\,k_P^{old}
(1)
wheremeaningunit
kPk_PTurbulent kinetic energy of cell Pm²/s²
kPoldk_P^{old}Value of the previous iterationm²/s²
aP,anba_P, a_{nb}Diagonal and neighbour coefficients of the kk matrixm³/s
bbSource terms (production and part of the dissipation)m⁵/s³
αk\alpha_kRelaxation factor-

Default and rule

Default
auto: 0.7 (SIMPLEC and plain SIMPLE), 0.9 (transonic SIMPLE)Computed by the programMeasured
Rule

Auto: 0.7 with SIMPLEC and with plain SIMPLE (incompressible and compressible); 0.9 with the transonic SIMPLE solver; not relaxed by the pseudo-transient solver; 0.7 after a divergence fallback.

Source

Validation on the two-inlet test muffler (see Pressure relaxation): with plain SIMPLE, kk and ω\omega at 0.5 gave a lower pressure residual than at 0.7 or 0.3 (2.3e-2 against 7.1e-2 and 4.2e-2 with U 0.5); with SIMPLEC, 0.7 and 0.9 both converged (1.6e-2 and 1.1e-2). The auto value 0.7 is the program's default for both couplings. Implicit relaxation: (Patankar and Spalding, 1972).

Valid range 0 < α ≤ 1

Values

0<αk≤10 < \alpha_k \le 1. Keep kk and ω\omega equal unless there is a reason not to.

References 1

  1. Patankar, S. V. and Spalding, D. B. (1972). A calculation procedure for heat, mass and momentum transfer in three-dimensional parabolic flows. International Journal of Heat and Mass Transfer, 15(10), 1787-1806. DOI 10.1016/0017-9310(72)90054-3