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Modélisation de l'écoulement diphasique dans les injecteurs Diesel

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CAV2001:sessionB6.005 3It can be clearly seen from figure 1 that the sound speed of the homogeneous mixture <strong>de</strong>creasesdramatically as soon as the fluid is not composed of a single phase. This can be explained by themultiple reflexions of the waves between the mixture’s components interfaces. As a matter of fact,10 4 Void fraction (−)10 3Sound velocity (m/s)10 210 110 010 −10 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1Fig. 1 – Sound speed, a, versus void fraction, α.we can almost consi<strong>de</strong>r that, as soon as cavitation appears in a numerical cell, the flow becomeslocally supersonic. We will see in sections 2.4.2 and 2.4.4 that this conclusion is very importantwith regards to boundary conditions.As we consi<strong>de</strong>r the flow as isentropic, we can assume that :a 2 = dPdρ . (7)Consi<strong>de</strong>ring the acoustic speed as constant in pure vapour and pure liquid, we can calculate theequation of state for the two-phase region H by integrating the expression 7 between the saturationpressure P sat l and the indicated pressure P (see figure 2) :⎧⎪⎨⎪⎩P = ρa 2 g if ρ < ρ gP = P sat l + ρ ga 2 gρ l a 2 l (ρ g − ρ l )ρ g2 a 2 g − ρ l2 a 2 lP = ρa 2 lif ρ > ρ l .log[ ]ρg a 2 g(ρ l + α(ρ g + ρ l ))ρ l (ρ g a 2 g − ρ l a 2 l ) if ρ g < ρ < ρ lThis equation is used in the co<strong>de</strong> to evaluate analytically P from ρ calculated by the continuityequation.2.3 Numerical schemeThe numerical scheme for advection consists in a quasi-second or<strong>de</strong>r upwind scheme (QSOU)as reported in Ams<strong>de</strong>n et al. 1989, which assures the monotonicity of the solution. That is to saythat no negative values (by oscillations) can be obtained, <strong>de</strong>spite pressure and <strong>de</strong>nsity ratios aretremendous. This is very important with regards to calculation robustness. Furthermore, as wehave to consi<strong>de</strong>r the transient behaviour of cavitation, the time advancement is ma<strong>de</strong> thanks to athird-or<strong>de</strong>r Runge-Kutta scheme.(∂ ρ∂ t) k ( ) kThe procedure is as follows : <strong>de</strong>fined at cell centers and ∂ ρU∂ t <strong>de</strong>fined at vertices arecalculated from equations 1 and 2 thanks to a finite-volume method. Then, according to Runge-(8)

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