The simple chemical reacting system (SCRS) is one of the combustion models for computational fluid dynamics. This model helps us to determine the process of combustion which is a vital phenomenon used in many engineering applications like aircraft engines, internal combustion engines, rocket engines, industrial furnaces, and power station combustors. The simple chemical reacting system (SCRS) refers the global nature of the combustion process considering only the final species concentrations. The detailed kinetics of the process is generally neglected and it postulates that combustion does proceed via a global one-step without intermediates. Infinitely fast chemical reaction is assumed with oxidants reacting in stoichiometric proportions to form products. SCRS considers the reaction to be irreversible i.e. rate of reverse reaction is presumed to be very low. 1 kg of fuel + s kg of oxidant → (1 + s) kg of products For the combustion of the methane gas the equation becomes CH4 + 2O2 → CO2 + 2H2O 1 mole of CH4 + 2 moles of O2 → 1 mole of CO2 + 2 moles of H2O The stoichiometric proportions of the above equation is given by 1 kg of CH4 + (64/16) kg of O2 → (1+ 64/16) kg of products The transport equations for the fuel and oxygen mass fractions are
d ( ρ m f u ) d t + d i v ( ρ m f u u ) = d i v ( R f u . g r a d m f u ) + S f u {\displaystyle {d(\rho m_{fu}) \over dt}+div(\rho m_{fu}u)=div(R_{fu}.gradm_{fu})+S_{fu}}
d ( ρ m o x ) d t + d i v ( ρ m o x u ) = d i v ( R o x . g r a d m o x ) + S o x {\displaystyle {d(\rho m_{ox}) \over dt}+div(\rho m_{ox}u)=div(R_{ox}.gradm_{ox})+S_{ox}}
Now consider a variable ‘ ϕ {\displaystyle \phi } ’ defined by
ϕ = s m f u − m o x {\displaystyle \phi =sm_{fu}-m_{ox}}
Also the mass transport coefficients, appearing in the transport equations are assumed to be a constant and are equal to ‘RΦ’ Now the transport equations of fuel and oxygen can be written as
d ( ρ ϕ ) d t + d i v ( ρ ϕ u ) = d i v ( R ϕ . g r a d ϕ ) + ( s . S f u − S o x ) {\displaystyle {d(\rho \phi ) \over dt}+div(\rho \phi u)=div(R_{\phi }.grad\phi )+(s.S_{fu}-S_{ox})}
Assuming the reaction to be one step, infinitely fast we can conclude s . S f u − S o x = 0 {\displaystyle s.S_{fu}-S_{ox}=0}
Now the transport equation reduces to
d ( ρ ϕ ) d t + d i v ( ρ ϕ u ) = d i v ( R ϕ . g r a d ϕ ) {\displaystyle {d(\rho \phi ) \over dt}+div(\rho \phi u)=div(R_{\phi }.grad\phi )}
Now defining the mixture fraction ‘f’, a non-dimensional variable in terms of ‘Φ’ we get
f = ϕ − ϕ 0 ϕ 1 − ϕ 0 {\displaystyle f={\frac {\phi -\phi _{0}}{\phi _{1}-\phi _{0}}}}
Where the suffix ‘1’ denotes the fuel stream and ‘0’ denotes oxygen stream. If the mixture contains only oxygen the mixture fraction ‘f’ is given by the value ‘0’ and if it contains only fuel it is given by ‘1’. Now substituting the value of ‘Φ’ in the above mixture fraction equation we get
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