Environmental Engineering Reference
In-Depth Information
steady-state fuel vapor conservation equation, but taking into account a fixed
droplet radius as boundary condition. Following a similar reasoning, provided
the evaporation process is fast compared to the transport of heat and mass to
the surface, the fuel mass fraction at the surface Y
s
can be obtained from equilib-
rium thermodynamics. The equilibrium vapor mole fraction at the surface, X
s
,at
saturation temperature T
sat
is obtained from the saturation pressure
p
sat
determined
by the Clausius
-
Clapeyron equation, relating saturation temperature and saturation
pressure:
X
s
=
p
sat
h
fg
R
u
=
1
T
boil
−
1
T
sat
p
atm
= exp
ð
Eq
:
4
:
34
Þ
MW
F
where h
fg
is the latent heat of vaporization of the fuel, R
u
is the universal gas constant,
and MW
F
is the MW of the fuel.
The vapor mass fraction is obtained using the relation between mole fraction and
mass fraction in a mixture of vapor and air:
MW
F
X
s
MW
F
+1
:
:
Y
s
=X
s
ð
Eq
4
35
Þ
ð
−
X
s
Þ
MW
air
Deviations from the phase equilibrium at the surface can occur when the evaporation
is very fast, occurring for small droplets and for droplets with a temperature very close
to the boiling point. Bellan and Summerfield (1978) have presented expressions for
evaporation rate taking into account nonequilibrium effects.
The solution of Equation (4.32) is (if
ρ
D
is assumed constant)
exp
½
− m
d
=
ð
4
π
r
d
ρ
D
Þ
ð
1
−
ð
r
d
=
r
Þ
Þ
−
1
Yr
ðÞ
=Y
s
+Y
b
−
ð
Y
s
Þ
for
r
≥
r
d
ð
Eq
:
4
:
36
Þ
exp
½
−
_
ð
m
d
=
4
π
r
d
ρ
D
Þ
−
1
From Equation (4.31) and Equation (4.36), it follows that
D
∂
Y
∂
1
r
2
m
d
= m
d
Y
s
+4
π
ρ
= m
d
Y
s
+ m
d
Y
s
−
ð
Y
b
Þ
ð
Eq
:
4
:
37
Þ
r
m
d
_
r
d
exp
−
−
1
4
π
r
d
ρ
D
This equation can be solved for
m
d
with the following result:
_
m
d
=
_
−
4
π
r
d
ρ
D
ln B
M
+1
ð
Þ
ð
Eq
:
4
:
38
Þ
Here, B
M
is the Spalding mass coefficient:
B
M
=
Y
s
−
Y
b
ð
Eq
:
4
:
39
Þ
1
−
Y
s
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