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Untitled - Aerobib - Universidad Politécnica de Madrid

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11.2. DIMENSIONLESS PARAMETERS OF AEROTHERMOCHEMISTRY 263<br />

b) Continuity equation.<br />

c) Momentum equation.<br />

d) Energy equation.<br />

( )<br />

1<br />

ρv<br />

2 v2 + c p T − qε<br />

e) Diffusion equation.<br />

ρv dε = w. (11.2)<br />

dx<br />

p + ρv 2 − 4 3 µ dv = i. (11.3)<br />

dx<br />

D<br />

v<br />

dY<br />

dx<br />

− λ dT<br />

dx − 4 dv<br />

µv = me. (11.4)<br />

3 dx<br />

− Y + ε = 0. (11.5)<br />

Be l 0 , ρ 0 , v 0 , w 0 , p 0 , µ 0 , c p0 , T 0 , λ 0 and D 0 characteristic values of the corresponding<br />

quantities and let us change the variables of the preceding system as follows<br />

x = l 0 x ′ , ρ = ρ 0 ρ ′ , v = v 0 v ′ , w = w 0 w ′ , p = p 0 p ′ ,<br />

µ = µ 0 µ ′ , c p = c p0 c ′ p, T = T 0 T ′ , λ = λ 0 λ ′ , D = D 0 D ′ .<br />

(11.6)<br />

Thus all the “prime” quantities are dimensionless. For ε and Y this change is<br />

not necessary since both are already dimensionless and their variation field has been<br />

selected from zero to one.<br />

When these new variables (11.6) are introduced into the preceding system it<br />

may be written as follows:<br />

a) Equation of mass conservation.<br />

ρ ′ v ′ =<br />

( m<br />

ρ 0 v 0<br />

)<br />

. (11.7)<br />

b) Continuity equation. ( )<br />

ρ0 v 0<br />

ρ ′ w ′ dε<br />

l 0 w 0 dx = w′ . (11.8)<br />

c) Momentum equation.<br />

( )<br />

p0<br />

ρ 0 v0<br />

2 p ′ + ρ ′ v ′ 2 4 −<br />

3<br />

d) Energy equation.<br />

ρ ′ v ′ [ 1<br />

2<br />

( v<br />

2<br />

0<br />

)<br />

v ′ 2 + c<br />

′<br />

c p0 T p T ′ −<br />

0<br />

(<br />

− 4 3<br />

(<br />

µ0<br />

) (<br />

µ ′ dv′<br />

ρ 0 v 0 l 0 dx ′ =<br />

( ) ] (<br />

q<br />

ε −<br />

c p0 T 0<br />

µ 0 v0<br />

2 )<br />

µ ′ v ′ dv′<br />

l 0 ρ 0 v 0 c p0 T 0<br />

i<br />

ρ 0 v 2 0<br />

)<br />

. (11.9)<br />

)<br />

λ 0 T 0<br />

λ ′ dT ′<br />

l 0 ρ 0 v 0 c p0 T 0 dx ′<br />

( )<br />

dx = me<br />

. (11.10)<br />

ρ 0 v 0 c p0 T 0

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