Combustion Stoichiometry
- To calculate the stoichiometric air requirement for combustion, we determine the amount of air (oxygen) needed to completely oxidize a given fuel without leaving any unburned fuel or excess oxygen.
- Let’s calculate this for a general fuel combustion process.
Steps for Stoichiometric Air Calculation
1. General Combustion Reaction:
For a hydrocarbon fuel of formula CxHy:
Cx Hy+νO2 →x CO2+y/2 *H2O
- (moles of oxygen) is given by:
νO2=x+y/4
2. Mass of Oxygen Required:
Each mole of O2 has a molar mass of 32 g/mol so the mass of oxygen required for one mole of fuel is:
mO2
3. Mass of Air Required:
Since air is 21% oxygen by volume (23.2% by mass), the mass of air required is:
Stoichiometric Air-to-Fuel Ratio (AFRst)
The air-to-fuel ratio at stoichiometry is the ratio of the mass of air required to the mass of the fuel:
AFRst = Mair_st/Mfuel
Example of Stoichiometric Air Calculations
Methane (CH4) Combustion
- Chemical Reaction:
CH4+2O2→CO2+2H2O
- νO2=2
- Molar mass of CH4: 16 g/mol
Methane gas combustion reaction in combustion chamber
Mass of Oxygen Required:
mO2=νO2×32=2×32=64 gm
Mass of Air Required:
Mair=mO2* 0.232=64* 0.232 ≈2 76 gm
Air-to-Fuel Ratio:
AFRst=mairmfuel=276/16≈17.25
Hydrogen (CH4) Combustion
- Chemical Reaction:
2H2+O2→2H2
- νO2=1
- Molar mass of H2: 2 g/mol
Mass of Oxygen Required:
mO2=νO2×32=1×32=32 gm
Mass of Air Required:
mair=mO2* 0.232
Air-to-Fuel Ratio:
AFRs
Ethanol (C2H5OH) Combustion
- Combustion reaction: C2H5OH+3O2→2CO2+3H2O
- x=2, y=6
Mass of oxygen required:
mO2=
Mass of air required:
mair=96/0.232≈414 gm
Air-to-Fuel Ratio:
AFRst=Mair/Mfuel=414/46≈9.0
Propane (C3H8) Combustion
- Combustion reaction: C3H8+5O2→3CO2+4H2O
- x=3, y=8y
- νO2=3+8/4
Mass of oxygen required:
mO2=5×32=160 gm
Mass of air required:
mair=160*0.232≈690 g
Air-to-Fuel Ratio:
AFRst=Mair/Mfuel
Summary of Stoichiometric Air-to-Fuel Ratios:
- These values represent the mass of air required for the complete combustion of 1 unit of fuel at stoichiometric conditions.
- Methane (CH4): AFRst≈17.25
- Hydrogen (H2): AFRst≈69.0
- Stoichiometric Air-Fuel Ratios for Hydrocarbon Fuels
Stoichiometric Air-Fuel Ratios for Hydrocarbon Fuels
| Fuel | Chemical Formula | Stoichiometric AFR (by mass) |
|---|---|---|
| Methane | CH4 | 17.2 |
| Ethane | C2H6 | 16.0 |
| Propane | C3H8 | 15.6 |
| Butane | C4H10 | 15.5 |
| Pentane | C5H12 | 15.4 |
| Hexane | C6H14 | 15.2 |
| Ethanol | C2H5OH | 9.0 |
| Gasoline | Approx. C8H18 | 14.7 |
| Diesel | Approx. C12H23 | 14.5 |
| Kerosene | Approx. C10H22 | 14.6 |
| Hydrogen | H2 | 34.5 |
Stoichiometric Mixture Fraction Calculation
- The stoichiometric mixture fraction (Zst) calculation depends on the stoichiometric air-fuel ratio, which defines the amount of air required for complete combustion of a given fuel.
- Let’s calculate it for methane (CH4) and pure hydrogen (H2) with air as the oxidizer.
Stoichiometric Mixture Fraction Formula:
Zst=1/(1+So/Sf)
Where:
- : Stoichiometric mass of oxidizer per unit mass of fuel.
- Sf: Stoichiometric mass of fuel per unit mass of oxidizer.
Breaking it Down:
sO=Air-to-Fuel Ratio at Stoichiometry (AFRst)
For air:
sO=(Mass of air/Mass of fuel)=(4.76*νO2*MWair)/(νF⋅MWF)
Where:
- : Stoichiometric oxygen requirement.
- : Fuel coefficient in the reaction.
- : Molar mass of the fuel (g/mol).
- : Molar mass of air, approximately 28.97 g/mol
- The factor 4.76 accounts for the ratio of air to oxygen (79%N2+21%O2)
Methane (CH4) Combustion
Combustion Reaction:
CH4+2 O2→CO2+2 H2O
- νO2=2
- νF=1
- MWCH4=16 g
Stoichiometric Air-to-Fuel Ratio (AFRst)
AFRst=4.76*2*28.97/1⋅16=17.19
Mixture Fraction:
Zst=1/(1+AFRst)=1/(1+17.19)
For Hydrogen (H2) Combustion
Combustion Reaction:
2 H2+O2→2 H2O2
- νO2=1
- MWH2=2 g/mol
Stoichiometric Air-to-Fuel Ratio (AFRst)
AFRst=4.76*1*28.97/(2*2)=
Mixture Fraction:
Zst=1/(1+AFRst_=
Summary of Stoichiometric Mixture Fractions:
- Methane (CH4): Zst
- Hydrogen (H2): Zst
These values are specific to the stoichiometric combustion of these fuels with air.
Scope of stichometry for CFD Simulations
- The stoichiometry of combustion plays a critical role in providing input data for Computational Fluid Dynamics (CFD) simulations, especially in modeling chemical reactions, energy transfer, and pollutant formation in combustion systems.
- Here’s an overview of its scope as a CFD data
Defining Combustion Chemistry
- Stoichiometric calculations define the chemical reaction equations for fuels and oxidizers, which are crucial in CFD models that simulate:
- Combustion reactions.
- Species transport (e.g., CO, CO2_2, H2O, NOx.
- Energy release and heat transfer.
- Example: For a hydrocarbon fuel, the stoichiometric air-to-fuel ratio helps establish the oxygen consumption and product formation for equilibrium calculations.
Setting Boundary Conditions
- Stoichiometric ratios influence key boundary condition parameters in CFD simulations:
- Inlet Conditions:
- Air-fuel mixture composition at the inlets.
- Equivalence ratio
- Outlet Conditions:
-
- Expected species concentrations (e.g., excess oxygen, unburned hydrocarbons) depend on stoichiometry.
-
Energy Source Term
Stoichiometric calculations provide the heat release rate, which is a function of:
- Fuel type and lower heating value (LHV).
- Combustion efficiency.
- Extent of reaction (stoichiometric or otherwise).
CFD uses this data to model thermal dynamics, such as:
- Temperature rise in the combustor.
- Heat transfer to walls or surroundings.
Application-Specific Scope
- Gas Turbines: Stoichiometry defines lean-premixed conditions for low-emission designs.
- IC Engines: Helps in simulating stratified charge combustion or fuel injection strategies.
- Industrial Boilers: Used for optimizing fuel-air supply for efficiency and minimal pollutants.
- Burners and Furnaces: Guides flame stability and energy efficiency analysis.
Uses Stoichiometry for CFD Simulations
- ANSYS Fluent: Utilizes stoichiometric data for premixed, non-premixed, and partially premixed combustion models.
- OpenFOAM: Uses mixture fraction and equivalence ratio in reacting flow solvers.
- COMSOL Multiphysics: Employs stoichiometric relationships for chemical species transport and energy balance in combustion simulations.