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Wind field simulations at Askervein hill - WindSim

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∂<br />

( ρε )<br />

∂t<br />

p<br />

∂<br />

+<br />

∂x<br />

i<br />

⎛<br />

⎜ ρε<br />

p<br />

⎝<br />

∂U<br />

∂x<br />

i<br />

ρν<br />

T<br />

−<br />

C<br />

( ε )<br />

p<br />

∂ε<br />

p<br />

⎞<br />

⎟<br />

ρ<br />

=<br />

∂x<br />

i ⎠ k<br />

p<br />

2<br />

2<br />

( C p + C p ε − C ε )<br />

p1 k p2<br />

k p p3<br />

p<br />

∂<br />

( ρε )<br />

∂t<br />

t<br />

∂<br />

+<br />

∂x<br />

i<br />

⎛ ∂U<br />

⎜ ρε<br />

t<br />

⎝ ∂xi<br />

ρν<br />

T<br />

−<br />

C<br />

∂ε<br />

C<br />

t<br />

⎞<br />

⎟ = ρ<br />

⎠<br />

2<br />

2<br />

t1ε<br />

p<br />

+ Ct2ε<br />

tε<br />

p<br />

− Ct3ε<br />

t<br />

( ε<br />

t<br />

) ∂x<br />

⎟<br />

i<br />

kt<br />

where C(ε p ), C(ε t ), C p1 , C p2 , C p3 , C t1 , C t2 and C t3 are constant model coefficients. The<br />

C p1 p k 2 /k p and C t1 ε 2 /k t terms can be interpreted as variable energy transfer functions. The<br />

former term increases the energy transfer r<strong>at</strong>e when production is high, and the second term<br />

increases the dissip<strong>at</strong>ion r<strong>at</strong>e when the energy transfer r<strong>at</strong>e is high.<br />

The model constants are given as:<br />

C(k p ) C(ε p ) C(k t ) C(ε p ) C p1 C t2 C t3 C 1 C t2 C t3<br />

0.75 1.15 0.75 1.15 0.21 1.24 1.84 0.29 1.28 1.66<br />

The eddy viscosity is computed from:<br />

ν<br />

T<br />

=<br />

C<br />

µ<br />

ε<br />

k<br />

t<br />

2<br />

The model may be used in combin<strong>at</strong>ion with equilibrium (GRND2) or non-equilibrium<br />

(GRND3) wall functions (see part 2.3.2.2).<br />

2.3. Numerical setup<br />

2.3.1. Calcul<strong>at</strong>ion domain<br />

The physical domain is discretised with a 54*44 grid covering an area of about 3000 meters in<br />

x and y directions. The height of the domain is fixed <strong>at</strong> 1100 meters, with a variable number<br />

of cells and a variable geometrical distribution, who are tested in this study.<br />

2.3.2. Boundary conditions<br />

2.3.2.1. Inflow<br />

Two different inlet profiles have been tested.<br />

First, inlet profiles for velocity, kinetic energy and dissip<strong>at</strong>ion r<strong>at</strong>e of kinetic energy are given<br />

by the following analytical expressions :<br />

U<br />

1<br />

=<br />

U<br />

κ<br />

* τ<br />

U = 1 0 m s<br />

k<br />

1<br />

⎛<br />

l n ⎜<br />

⎝<br />

z<br />

z<br />

0<br />

⎞<br />

⎟<br />

⎠<br />

for z

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