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The computation of turbulent natural convection flows - Turbulence ...

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Wall Functions 104<br />

In the case <strong>of</strong> prescribed wall heat flux, the wall temperature can be calcu-<br />

lated by:<br />

where<br />

Θwall = Θn − Prny ∗ n<br />

µn<br />

<br />

Cthy∗ n<br />

2 +Ath<br />

<br />

Prny<br />

+bµ<br />

∗2<br />

n<br />

2µ<br />

Ath = − qwall<br />

cp<br />

µn<br />

<br />

ρn kp<br />

<br />

Cthy∗ n<br />

3 +Ath<br />

<br />

(4.46)<br />

(4.47)<br />

In the case <strong>of</strong> prescribed wall temperature, the wall heat flux can be calcu-<br />

lated as:<br />

where<br />

qwall = − ρncp<br />

<br />

kp<br />

µn<br />

Ath<br />

Ath = (Θn −Θwall) µn Cth − Prn 2 y∗2 n +bµ<br />

y ∗ n<br />

− 1<br />

2<br />

bµy ∗2<br />

n<br />

Cthy ∗3<br />

n<br />

6<br />

(4.48)<br />

(4.49)<br />

4.2.4 Hydrodynamic Wall Function When the Near Wall Cell<br />

Is Thicker Than the Viscous Sublayer<br />

We now integrate the simplified wall-parallel momentum equation over<br />

the near-wall cell in a similar manner to that just outlined for the temperature<br />

equation. First we convert the simplified differential transport equation for<br />

momentum into y ∗ coordinates:<br />

or<br />

where<br />

∂<br />

∂y∗ <br />

(µ+µt) ∂U<br />

∂y∗ <br />

= µ2 υ<br />

ρ 2 υ kP<br />

+ µ2 υ<br />

ρ 2 υ kP<br />

∂(ρUU)<br />

∂x<br />

+ ∂(ρVU)<br />

∂y<br />

+ dP<br />

<br />

dx P<br />

[−ρrefgβ(Θ−Θref)] (4.50)<br />

∂<br />

∂y∗ <br />

(µ+µt) ∂U<br />

∂y∗ <br />

= C +b(Θ−Θref) (4.51)<br />

b = − µ2υ ρ2 ρrefgβ (4.52)<br />

υkP

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