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Untitled - Aerobib - Universidad Politécnica de Madrid

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3.7. ONE-DIMENSIONAL MOTIONS 73<br />

reduces to<br />

ρ ∂v ∂v<br />

+ ρv<br />

∂t ∂x = − ∂p<br />

∂x + 4 3<br />

∂<br />

∂x<br />

(<br />

µ ∂v )<br />

. (3.52)<br />

∂x<br />

Energy equation<br />

Equation (3.34) reduces to<br />

ρ ∂u ∂u<br />

+ ρv<br />

∂t<br />

∂x = − p ∂v<br />

∂x + 4 ( ∂v<br />

3 µ ∂x<br />

− ∂ (<br />

λ ∂T<br />

∂x ∂x<br />

) 2<br />

)<br />

− ∂<br />

∂x<br />

(<br />

ρ ∑ i<br />

Y i h i v di<br />

)<br />

Or if it is <strong>de</strong>ci<strong>de</strong>d to use the total energy equation (3.38) it takes the form<br />

ρ ∂ (h + 1 )<br />

∂t 2 v2 + ρv ∂ (h + 1 )<br />

∂x 2 v2 = ∂p<br />

∂t + 4 (<br />

∂<br />

µv ∂v )<br />

3 ∂x ∂x<br />

+ ∂ (<br />

λ ∂T ) (<br />

− ∂ ρ ∑ )<br />

Y i h i v di .<br />

∂x ∂x ∂x<br />

i<br />

.<br />

(3.53)<br />

(3.54)<br />

The system of equations (3.49), (3.50), (3.52) and (3.53), or (3.54), must be<br />

completed with the following equations.<br />

Total mass fraction equation<br />

∑<br />

Y i = 1. (3.55)<br />

i<br />

Diffusion equations<br />

The system of equations (3.8) which gives the diffusion velocities reduces to<br />

∑<br />

[ (<br />

Y j vdi − v dj 1 ∂Y i<br />

+<br />

M j D ij Y i ∂x − 1 )<br />

∂Y j<br />

Y j ∂x<br />

j<br />

+ M j − M i<br />

M m<br />

( )] 1 ∂p<br />

= 0, (i = 1, 2, . . . , l),<br />

p ∂x<br />

∑<br />

Y i v di = 0.<br />

i<br />

(3.56)<br />

State equation<br />

The state equation is, by assumption, that of i<strong>de</strong>al gases<br />

p<br />

ρ = R mT. (3.39)

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