Chemical Reactions
Chemical Reactions
Chemical Reactions
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15.5 Adiabatic Flame Temperature<br />
Adiabatic Flame Temperature = Maximum limit of combustion<br />
gas temperature of each Air – Fuel mixture<br />
(Adiabatic Flame Temperature = Combustion Temperature)<br />
Q cv =0,W cv =0 ,∆KE=,<br />
KE=∆PE=0 :<br />
1 st law<br />
_<br />
_<br />
Qcv<br />
+ ΣNi<br />
hi<br />
= Wcv<br />
+ ΣNe<br />
he<br />
ΣN<br />
R<br />
{<br />
_<br />
o<br />
h f<br />
_<br />
ΣN<br />
i<br />
_<br />
o<br />
_<br />
h<br />
+ ( h−<br />
h )}<br />
i<br />
= ΣN<br />
R<br />
e<br />
= ΣN<br />
_<br />
h<br />
P<br />
e<br />
{<br />
_<br />
o<br />
h f<br />
To Calculate the adiabatic flame temperature, T P<br />
1. Write the combustion equation<br />
2. Apply energy balance (1 st law)<br />
3. Solving by trial-and<br />
and-error technique by assume a value of T P<br />
get values…and<br />
and<br />
substitute in (2) ….LHS = RHS ..if not try new T P<br />
….. (in good procedure we can<br />
interporate the former value to get the right value of T P<br />
_<br />
_<br />
o<br />
+ ( h−<br />
h )}<br />
P<br />
• What is your first guess of T<br />
• What should be the 2 nd trial.<br />
• How about the 3 rd , 4 th ......<br />
• When/how to interporate<br />
a<br />
b<br />
<br />
Trail and error procedure<br />
LHS - RHS = Error<br />
T<br />
T 2<br />
T c<br />
Interporation<br />
T b<br />
T a<br />
c<br />
T 2<br />
E 2<br />
T a -E a<br />
T b -E b<br />
T 2<br />
0.0<br />
T c +E c<br />
T 2 = 342 o C<br />
m i =1.263 kg<br />
-E a -E b E = 0<br />
+E c<br />
Error<br />
18