GAS POWER CYCLES 649
dharm
\M-therm\Th13-3.pm5
∴ T 2 = 300 × 2.954 = 886.2 K
p
p
v
v
2
1
1
2
=F 1514
HG
I
KJ
=
γ
(). ⇒ p 2 = 44.3 p 1
Constant pressure process 2-3 :
p
T
p
T
2
2
3
3
=
or T 3 = T 2 ×
p
p
3
2
= 886.2 ×
70
44 3
1
1
p
. p
= 1400 K
Also, Heat added at constant volume = Heat added at constant pressure ...(Given)
or cv (T 3 – T 2 ) = cp (T 4 – T 3 )
or T 3 – T 2 = γ (T 4 – T 3 )
or T 4 = T 3 +
TT 32 −
γ
= 1400 +
1400 886 2
14
−.
.
= 1767 K.
Constant volume process 3-4 :
v
T
v
T
3
3
4
4
= ⇒ v
v
T
T
4
3
4
3
1767
1400
== = 1.26
Also,
v
v
v
v
4
3
4
115
=
(/ )
= 1.26 or v 4 = 0.084 v 1
Also, v 5 = v 1
Adiabatic expansion process 4-5 :
T
T
v
v
v
v
4
5
5
4
1
1
1
14 1
0 084
=
F
HG
I
KJ
=
F
HG
I
KJ
γ−−
.
.
= 2.69
∴ T 5 = T^4
269
1767
269
656 9
..
==.K
∴ηair-standard =
Work done
Heat supplied =
Heat supplied Heat rejected
Heat supplied
−
= 1 – Heat rejected
Heat supplied
= 1 –
cT T
cT T c T T
v
v p
()
()()
51
32 43
−
−+ −
= 1 –
()
()()
TT
TT TT
51
32 43
−
−+ −γ
= 1 –
()
()()
656.9 300
1400 886.2 4 1767 1400
−
−+ −1.
= 0.653 or 65.3%. (Ans.)
Reasons for actual thermal efficiency being different from the theoretical value :
- In theoretical cycle working substance is taken air whereas in actual cycle air with fuel
acts as working substance. - The fuel combustion phenomenon and associated problems like dissociation of gases,
dilution of charge during suction stroke, etc. have not been taken into account.