Abbreviations
- BDC:
-
Bottom dead center
- EGR:
-
Exhaust gas recirculation
- HCCI:
-
Homogeneous charge compression ignition
- IC:
-
Internal combustion
- LTC:
-
Low-temperature combustion
- TDC:
-
Top dead center
Abbreviations
- η c :
-
Combustion efficiency
- η f :
-
Fuel conversion efficiency
- η f,b :
-
Brake fuel conversion efficiency
- η f,i,:
-
Indicated fuel conversion efficiency
- η m :
-
Mechanical efficiency
- η th :
-
Thermal efficiency
- η th,Carnot :
-
Thermal efficiency of the ideal Carnot cycle
- η th,Otto :
-
Thermal efficiency of the ideal heat engine Otto cycle
- η v :
-
Volumetric efficiency
- γ :
-
Ratio of specific heats
- γ b :
-
Ratio of specific heats of the burned mixture
- φ :
-
Fuel-air equivalence ratio. For φ <1 mixture is lean. For φ = 1, mixture is stoichiometric. For φ >1, mixture is rich. Note that φ is the inverse of the often-used air-fuel equivalence ratio or λ.
- ρ a,i :
-
Inlet air density
- τ :
-
Engine torque
- BMEP:
-
Brake mean effective pressure
- C p,b :
-
Constant pressure specific heat of the burned mixture
- C v,b :
-
Constant volume specific heat of the burned mixture
- f :
-
Residual fraction
- f final :
-
Final calculated residual fraction
- f final – 1 :
-
Previous iteration residual fraction to final calculated residual fraction
- (F/A):
-
Fuel-air ratio
- FMEP:
-
Friction mean effective pressure
- h 1 :
-
Specific enthalpy at state 1
- h 2 :
-
Specific enthalpy at state 2
- h 3 :
-
Specific enthalpy at state 3
- h 3a :
-
Specific enthalpy at state 3a
- h 5 :
-
Specific enthalpy at state 5
- h 6 :
-
Specific enthalpy at state 6
- h e :
-
Specific enthalpy of exhaust mixture
- h i :
-
Specific enthalpy of inlet mixture
- IMEPg :
-
Gross indicated mean effective pressure
- IMEPn :
-
Net indicated mean effective pressure
- m :
-
Mass
- m 1 :
-
Mass at state 1
- m 2 :
-
Mass at state 2
- m 3 :
-
Mass at state 3
- m 4 :
-
Mass at state 4
- m 6 :
-
Mass at state 6
- m a :
-
Mass of air
- m f :
-
Mass of fuel
- m r :
-
Residual mass
- m total :
-
Total mass
- \( {\dot{\mathbf{m}}}_{\mathrm{a}} \) :
-
Mass flow rate of air
- \( {\dot{\mathbf{m}}}_{\mathbf{f}} \) :
-
Mass flow rate of fuel
- MEP:
-
Mean effective pressure
- M b :
-
Molecular weight of the burned mixture
- n R :
-
Number of revolutions per engine cycle
- N :
-
Engine speed
- \( \overline{\mathbf{R}} \) :
-
Universal gas constant
- R :
-
Gas constant
- R 5 :
-
Gas constant of mixture at state 5
- R 6 :
-
Gas constant of mixture at state 6
- R e :
-
Gas constant of exhaust mixture
- P :
-
Cylinder pressure or power
- P 1 :
-
Pressure at state 1
- P 2 :
-
Pressure at state 2
- P 3 :
-
Pressure at state 3
- P 3a :
-
Pressure at state 3a
- P 4 :
-
Pressure at state 4
- P 5 :
-
Pressure at state 5
- P 6 :
-
Pressure at state 6
- P 7 :
-
Pressure at state 7
- P b :
-
Brake power
- P e :
-
Exhaust pressure
- P i :
-
Inlet (initial) pressure
- P in :
-
Net indicated power
- P limit :
-
Limit pressure
- PMEP:
-
Pumping mean effective pressure
- 1 Q 2 :
-
Heat transfer of process 1-2
- 6 Q 1 :
-
Heat transfer for process 6-1
- Q HV :
-
Heating value of fuel
- Q HV,f :
-
Heating value of fuel
- Q HV,i :
-
Heating value of specie i
- r c :
-
Compression ratio
- s 1 :
-
Entropy at state 1
- s 2 :
-
Entropy at state 2
- s 3 :
-
Entropy at state 3
- s 4 :
-
Entropy at state 4
- s 5 :
-
Entropy at state 5
- T 1 :
-
Temperature at state 1
- T 4 :
-
Temperature at state 4
- T 5 :
-
Temperature at state 5
- T 6 :
-
Temperature at state 6
- T cv,adiabatic :
-
Constant volume adiabatic flame temperature
- T e :
-
Exhaust temperature
- T H :
-
Temperature of a source reservoir
- T i :
-
Inlet temperature
- T L :
-
Temperature of a sink reservoir
- T r :
-
Residual fraction temperature
- u 1 :
-
Specific internal energy at state 1
- u 2 :
-
Specific internal energy at state 2
- u 3 :
-
Specific internal energy at state 3
- u 3a :
-
Specific internal energy at state 3a
- u 4 :
-
Specific internal energy at state 4
- U 1 :
-
Internal energy at state 1
- U 2 :
-
Internal energy at state 2
- U 3 :
-
Internal energy at state 3
- U 4 :
-
Internal energy at state 4
- v 1 :
-
Specific volume at state 1
- v 2 :
-
Specific volume at state 2
- v 3 :
-
Specific volume at state 3
- v 3a :
-
Specific volume at state 3a
- v 4 :
-
Specific volume at state 4
- V :
-
Cylinder volume
- V 1 :
-
Volume at state 1
- V 2 :
-
Volume at state 2
- V 3 :
-
Volume at state 3
- V 5 :
-
Volume at state 5
- V 6 :
-
Volume at state 6
- V d :
-
Displaced volume
- V max :
-
Maximum cylinder volume
- V min :
-
Minimum cylinder volume
- W :
-
Thermodynamic work
- 1 W 2 :
-
Work for process 1-2
- 2 W 3 :
-
Work for process 2-3
- 3 W 4 :
-
Work for process 3-4
- 4 W 5 :
-
Work for process 4-5
- 5 W 6 :
-
Work for process 5-6
- 6 W 1 :
-
Work for process 6-1
- W b :
-
Brake work
- W f :
-
Friction work
- W gross :
-
Gross work
- W ig :
-
Gross indicated work
- W in :
-
Net indicated work
- W ip :
-
Pump work
- W net :
-
Net work
- x i :
-
Mole fraction of specie i
- y i :
-
Mass fraction of specie i
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Jacobs, T.J. (2018). Internal Combustion Engines, Developments in. In: Meyers, R. (eds) Encyclopedia of Sustainability Science and Technology. Springer, New York, NY. https://doi.org/10.1007/978-1-4939-2493-6_430-3
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