526 ENGINEERING THERMODYNAMICS
dharm
\M-therm\Th11-2.pm5
O 2 =
075
19 85
.
.
× 100 = 3.78%. (Ans.)
N 2 =
14 1
19 85
.
.
× 100 = 71.03%. (Ans.)
The total dry moles = 2 + 0.75 + 14.1 = 16.85
Hence dry analysis is :
CO 2 =
2
16 85.
× 100 = 11.87%. (Ans.)
O 2 =^075
16 85
.
.
× 100 = 4.45%. (Ans.)
N 2 = 14 1
16 85
.
.
× 100 = 83.68%. (Ans.)
Considering a mixture strength of 130% :
Now, 1.3 = Stoichiometric ratio
Actual A/F ratio
∴ Actual A/F ratio =
896
13
.
.
= 6.89/1. (Ans.)
This means that
1
13.
or 0.769 of the stoichiometric air is supplied. The combustion cannot
be complete, as the necessary oxygen is not available. It is usual to assume that all hydrogen is
burned to H 2 O, since hydrogen atoms have a greater affinity for oxygen than carbon atoms. The
carbon in the fuel will burn to CO and CO 2 , but the relative proportions have to be determined.
Let, a = Number of moles of CO 2 in the products, and
b = Number of moles of CO in the products.
Then the combustion equation is as follows :
C 2 H 6 O + 0.769 3379
(^2221)
F ON+×
HG
I
KJ
→ a CO 2 + b CO + 3H 2 O + 0.769 × 3 ×^79
21
N 2
To find a and b a balance of carbon and oxygen atoms can be made,
i.e., Carbon balance :
2 = a + b ...(i)
and Oxygen balance :
1 + 2 × 0.769 × 3 = 2a + b + 3
or 2.614 = 2a + b ...(ii)
From eqns. (i) and (ii), we get
a = 0.614, b = 1.386
i.e., The products are : 0.614 moles CO 2 + 1.386 moles CO + 3 moles H 2 O + 8.678 moles N 2
The total moles = 0.614 + 1.386 + 3 + 8.678 = 13.678.
Hence wet analysis is :
CO 2 =
0 614
13 678
.
.
× 100 = 4.49%. (Ans.)
CO = 1 386
13 678
.
.
× 100 = 10.13%. (Ans.)