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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