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Synthetic Inflow Condition for Large Eddy Simulation (Synthetic - KTH

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and<br />

2.3 Numerical Method<br />

CHAPTER 2. BACKGROUND<br />

C 2 m ≈ 10.6C 2 s ≈ 0.58 (2.20)<br />

Among the important number of numerical methods simulating the viscous fluid,<br />

some of them will be presented on this section taken from the Ref.[6]. But firstly<br />

we need to define the hypotheses used <strong>for</strong> external aerodynamics which are the<br />

followings:<br />

• The air is considered as being a perfect gas<br />

• The kinetic viscosity of the air depends only on the temperature. Exemple:<br />

the law of Sutherland<br />

µ<br />

µ∞<br />

� �3/2 T T∞ + S1<br />

=<br />

T∞ T + S1<br />

(2.21)<br />

Where T is the temperature, µ∞ the kinetic viscosity <strong>for</strong> the reference temperature<br />

T∞ and S1 a constant (110 · 3 ž <strong>for</strong> air).<br />

• The conductive heat flux −→ q is given by the Fourier law<br />

−→ q = −λ −−→<br />

gradT (2.22)<br />

With these hypotheses, the Navier-Stokes equations are written:<br />

∂ −→ W<br />

∂t<br />

With −→ ⎜<br />

W the vector of the conservative variables ⎜<br />

⎝<br />

+ divF = 0 (2.23)<br />

⎛<br />

ρ<br />

ρu<br />

ρv<br />

ρw<br />

ρE<br />

⎞<br />

⎟ where E is the kinetic<br />

⎟<br />

⎠<br />

energy, F the flux matrice, F equals to F = f − fv where f is the matrice of the<br />

convectiv flux and fv is the matrix of the viscous flux.<br />

8

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