G equation
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Combustion Combustion, or burning, is a high-temperature exothermic redox chemical reaction between a fuel (the reductant) and an oxidant, usually atmospheric oxygen, that produces oxidized, often gaseous products, in a mixture termed as smoke. Combus ...
, G equation is a scalar G(\mathbf,t) field equation which describes the instantaneous flame position, introduced by Forman A. Williams in 1985 in the study of premixed turbulent combustion. The equation is derived based on the
Level-set method Level-set methods (LSM) are a conceptual framework for using level sets as a tool for numerical analysis of surfaces and shapes. The advantage of the level-set model is that one can perform numerical computations involving curves and surfaces o ...
. The equation was studied by George H. Markstein earlier, in a restrictive form.


Mathematical descriptionWilliams, Forman A. "Combustion theory." (1985).

The G equation reads as :\frac + \mathbf\cdot\nabla G = U_L , \nabla G, where *\mathbf is the flow velocity field *U_L is the local burning velocity The flame location is given by G(\mathbf,t)=G_o which can be defined arbitrarily such that G(\mathbf,t)>G_o is the region of burnt gas and G(\mathbf,t) is the region of unburnt gas. The normal vector to the flame is \mathbf=-\nabla G /, \nabla G, .


Local burning velocity

The burning velocity of the stretched flame can be derived by subtracting suitable terms from the unstretched flame speed, for small curvature and small strain, as given by :U_L = S_L - S_L \mathcal \kappa - \mathcal S where *S_L is the burning velocity of unstretched flame *S=-\mathbf\cdot\nabla\mathbf\cdot\mathbf is the term corresponding to the imposed
strain rate In materials science, strain rate is the change in strain ( deformation) of a material with respect to time. The strain rate at some point within the material measures the rate at which the distances of adjacent parcels of the material change ...
on the flame due to the flow field *\mathcal is the Markstein length, proportional to the laminar flame thickness \delta_L, the constant of proportionality is Markstein number \mathcal *\kappa = \nabla\cdot\mathbf = -\frac is the flame curvature, which is positive if the flame front is convex with respect to the unburnt mixture and vice versa.


A simple example - Slot burner

The G equation has an exact expression for a simple slot burner. Consider a two-dimensional planar slot burner of slot width b with a premixed reactant mixture is fed through the slot with constant velocity \mathbf=(0,U), where the coordinate (x,y) is chosen such that x=0 lies at the center of the slot and y=0 lies at the location of the mouth of the slot. When the mixture is ignited, a flame develops from the mouth of the slot to certain height y=L with a planar conical shape with cone angle \alpha. In the steady case, the G equation reduces to :U\frac = U_L \sqrt If a separation of the form G(x,y) = y + f(x) is introduced, the equation becomes :U = U_L\sqrt, \quad \text \quad \frac = \frac which upon integration gives :f(x) = \frac, x, + C, \quad \Rightarrow \quad G(x,y) = \frac, x, + y+ C Without loss of generality choose the flame location to be at G(x,y)=G_o=0. Since the flame is attached to the mouth of the slot , x, = b/2, \ y=0, the boundary condition is G(b/2,0)=0, which can be used to evaluate the constant C. Thus the scalar field is :G(x,y) = \frac\left(, x, - \frac\right) + y At the flame tip, we have x=0, \ y=L, \ G=0 , the flame height is easily determined as :L = \frac and the flame angle \alpha is given by :\tan \alpha = \frac = \frac Using the trigonometric identity \tan^2\alpha = \sin^2\alpha/\left(1-\sin^2\alpha\right), we have :\sin\alpha = \frac


References

{{Reflist, 30em Fluid dynamics Combustion