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Thermodynamic Cycles
Air-standard analysis is a simplification of the real cyclethat includes the following assumptions:
1) Working fluid consists of fixed amount of air (ideal gas)
2) Combustion process represented by heat transfer into and out of the cylinder from an external source
3) Differences between intake and exhaust processes not considered (i.e. no pumping work)
4) Engine friction and heat losses not considered
SI Engine Cycle vs Air Standard Otto Cycle
A I R
CombustionProducts
Ignition
IntakeStroke
FUEL
Fuel/AirMixture
AirTC
BC
CompressionStroke
PowerStroke
ExhaustStroke
Qin Qout
CompressionProcess
Const volume heat addition
Process
ExpansionProcess
Const volume heat rejection
Process
ActualCycle
OttoCycle
Process 1 2 Isentropic compressionProcess 2 3 Constant volume heat additionProcess 3 4 Isentropic expansionProcess 4 1 Constant volume heat rejection
v2TC
TCv1BC
BC
Qout
Qin
Air-Standard Otto cycle
3
4
2
1
v
v
v
vr
Compression ratio:
First Law Analysis of Otto Cycle
12 Isentropic Compression
)()( 12 m
W
m
Quu in
rv
v
v
v
r
r 1
1
2
1
2 2
1
1
2
1
2
1
11
2
22
v
v
T
T
P
P
T
vP
T
vPR
AIR
)( 12 uum
Win
First Law Analysis of Otto Cycle
23 Constant Volume Heat Addition
m
W
m
Quu in )()( 23
)( 23 uum
Qin
2
3
2
3
3
3
2
2
T
T
P
P
RT
P
RT
Pv
AIRQin
TC
3 4 Isentropic Expansion
AIR)()( 34 m
W
m
Quu out
)( 43 uum
Wout
rv
v
v
v
r
r 3
4
3
4
4
3
3
4
3
4
3
33
4
44
v
v
T
T
P
P
T
vP
T
vP
First Law Analysis of Otto Cycle
4 1 Constant Volume Heat Removal
AIRQoutm
W
m
Quu out )()( 41
)( 14 uum
Qout
1
1
4
4
1
1
4
4
T
P
T
P
RT
P
RT
Pv
BC
First Law Analysis of Otto Cycle
23
1243
uu
uuuu
Q
WW
Q
W
in
inout
in
cycleth
23
14
23
1423 1uu
uu
uu
uuuuth
Cycle thermal efficiency:
Net cycle work:
1243 uumuumWWW inoutcycle
First Law Analysis
• For a cold air-standard analysis the specific heats are assumed to be constant evaluated at ambient temperature values (k = cp/cv = 1.4).
• For the two isentropic processes in the cycle, assuming ideal gas with constant specific heat using yields:
Cold Air-Standard Analysis
1 2 : 11
2
1
1
2
k
k
rv
v
T
T k
k
P
P
T
T1
1
2
1
2
3 4 : 11
4
3
3
4 1
kk
rv
v
T
T k
k
P
P
T
T1
3
4
3
4
12
1
23
14 111
)(
)(1
kv
v
const cth rT
T
TTc
TTc
V
RTPvconstPvk .
Effect of Specific Heat Ratio
1
11 k
const cth r
V
Specific heat ratio (k)
Cylinder temperatures vary between 20K and 2000K where 1.2 < k < 1.4