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9.3.1 Closure for ECFM Source Terms

$P_1$ represents the production of flame area density by turbulent flame stretching, and is modeled as


 P_1 = \alpha_1 K_t = \alpha_1 \frac{\epsilon}{k} \left[ (1-\alpha_0) + \alpha_0 \Gamma_K \right] (9.3-2)

where $K_t$ is a turbulent time scale and $\alpha_1$ is a constant with a default value of 1.6. The constant $\alpha_0$ (default of 1) is a user-specified linear blending between the Intermediate Turbulent Net Flame Stretch (ITNFS) term, $\Gamma_K$, for low turbulence levels at $\alpha_0 = 1$, and a straightforward turbulent time scale source when $\alpha_0 = 0$ for high turbulence levels.

The ITNFS term, $\Gamma_K$, can be specified either as a constant or calculated as a function of the two parameters $u'/U_l$ and $l_t/\delta_L^0$, where $u'$ is the turbulent velocity fluctuation, $U_l$ is the laminar flame speed, $l_t$ is the integral turbulent length scale and $\delta_L^0$ is the laminar flame thickness.

The expression for $\Gamma_K$ is given by:


 \log_{10}(\Gamma_K) = - \frac{1}{(s+0.4)} \exp \left(- (s+0... ...\left(\sigma_1 \left(\frac{u'}{U_l} \right) s - 0.11 \right) (9.3-3)

where $s$ is defined as


 s = \log_{10} \left(\frac{l_t}{\delta_l^0} \right) (9.3-4)

and $\sigma_1$ is


 \sigma_1 \left(\frac{u'}{U_l} \right) = \frac{2}{3} \lef... ... \left(\frac{u'}{U_l} \right)^{\frac{1}{3}} \right) \right) (9.3-5)

The ITNFS term, $\Gamma_K$, is sensitive to the laminar flame thickness. ANSYS FLUENT provides several options for the calculation of this quantity:

The term $P_2$ in Equation  9.3-1 models the influence of dilatation on the production of flame area density. The term is given by


 P_2 = \alpha_2 \frac{2}{3} \nabla \cdot (\rho \vec{u}) (9.3-9)

where the constant $\alpha_2$ has a default of 1.

The term $P_3$ models the effect of thermal expansion of the burned gas on the flame area density, and is given by


 P_3 = \alpha_3 \frac{\rho_u}{\rho_b} U_l \frac{1-c}{c} \Sigma (9.3-10)

where $\alpha_3$ is 1 by default.

The flame area destruction term $D$ is modeled as


 D = \beta U_l \frac{\Sigma^2}{1-c} (9.3-11)

where $\beta$ is a constant with a default value of 1.

As formulated, the model can become singular for $c=0$ and $c=1$, which is handled by limiting $c$. Further, the production terms $P_1$ and $P_2$ can be non-zero in regions where the mixture is outside the flammability limits, which is unphysical. Accordingly, ANSYS FLUENT sets the production terms to zero when the laminar flame speed is less than a very small value. The stability of the solution is enhanced by ensuring that the laminar flame speed in the destruction term is always greater than a small, finite value. Inspection of the function for $\Gamma_K$ shows that a singularity exists in Equation  9.3-3 for $s$ = -0.4 which can occur when the turbulent integral length scale is small compared to the laminar flame thickness. To prevent the singularity, the quantity $(s + 0.4)$ is limited to a small positive number. This results in a small net turbulent flame stretch term in laminar zones. These numerical limiting constants can be adjusted in the TUI.


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