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Wind field simulations at Askervein hill - WindSim

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ν T<br />

= l m<br />

U<br />

PHOENICS provides mixing-length expressions for use in simple geometries with zero- and<br />

one-equ<strong>at</strong>ion turbulence models which apply in the fully turbulent part of the flow, excluding<br />

the sublayer and buffer layer close to the wall. These expressions can be modified to make<br />

them applicable over the entire boundary layer, by using extensions which allow the<br />

influence of viscous effects very close to the wall. One such extension is th<strong>at</strong> proposed by<br />

Van Driest [1956], which takes the form:<br />

l<br />

m<br />

= l<br />

m0<br />

⎛ ⎛<br />

⎜1<br />

− exp⎜<br />

⎝ ⎝<br />

y<br />

A<br />

+<br />

+<br />

⎞⎞<br />

⎟⎟<br />

⎠⎠<br />

Uτ<br />

y<br />

g<br />

where l m0 is the unmodified mixing length, y + = and A+= 26.0. Here, y g is the normal<br />

ν<br />

τ<br />

w<br />

distance from the wall to the grid node, U τ is the friction velocity <strong>at</strong> the wall U<br />

τ<br />

= and ν<br />

ρ<br />

is the laminar kinem<strong>at</strong>ic viscosity.<br />

In general the damping constant A+ is not constant, and proposals may be found in the<br />

liter<strong>at</strong>ure which employ a functional rel<strong>at</strong>ionship for A+ so as to account for strong pressure<br />

gradients, mass transfer, compressibility, etc.<br />

2.2.2. k-ε model<br />

The k-ε model can also be used to close the set of equ<strong>at</strong>ions. It uses the dissip<strong>at</strong>ion r<strong>at</strong>e of<br />

turbulent kinetic energy ε.<br />

It is obvious th<strong>at</strong> the k-ε model can not predict all the details of the flow with accuracy.<br />

Nevertheless, experience proves th<strong>at</strong> this choice provides r<strong>at</strong>her good results, even in complex<br />

cases such as separ<strong>at</strong>ion (T.UTNES and K.J. EIDSVIK, 1996). This model is widely used in<br />

engineering applic<strong>at</strong>ions and proves to be well documented.<br />

The k-ε model provides the following equ<strong>at</strong>ions for k and ε :<br />

νT c k 2<br />

=<br />

µ<br />

ε<br />

( U k i )<br />

∂<br />

∂ ⎛ ν<br />

T ∂ k ⎞<br />

=<br />

ε<br />

∂ x ∂ x ⎜ σ ∂ x ⎟ + P −<br />

i<br />

i ⎝ k i ⎠ k<br />

∂<br />

∂ ⎛ ν ∂ ε ⎞ ε<br />

∂<br />

( U ε<br />

T<br />

x i ) = ⎜ ⎟ c<br />

∂ x ⎜ σ ∂ x ⎟ + ε k P c<br />

k<br />

− ε<br />

i i ⎝ ε i ⎠<br />

1 2<br />

ε<br />

2<br />

k<br />

This closure introduces several constants which are given two different sets of values.<br />

The standard values have been tuned to fit some basic flow problems such as, shear layer in<br />

local equilibrium, decaying grid turbulence and a boundary layer where logarithmic velocity<br />

profile prevails. The model constants can be adjusted in order to mimic other flow regimes.<br />

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