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Mixture fraction

From Wikipedia, the free encyclopedia

Mixture fraction (Z{\displaystyle Z}) is a quantity used incombustion studies that measures themass fraction of one stream of a mixture formed by two feed streams, one the fuel stream and the other the oxidizer stream.[1][2] Both the feed streams are allowed to have inert gases.[3] The mixture fraction definition is usually normalized such that it approaches unity in the fuel stream and zero in the oxidizer stream.[4] The mixture-fraction variable is commonly used as a replacement for the physical coordinate normal to the flame surface, in nonpremixed combustion.

Definition

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Assume a two-stream problem having one portion of the boundary the fuel stream with fuel mass fractionYF=YF,F{\displaystyle Y_{F}=Y_{F,F}} and another portion of the boundary the oxidizer stream with oxidizer mass fractionYO=YO,O{\displaystyle Y_{O}=Y_{O,O}}. For example, if the oxidizer stream is air and the fuel stream contains only the fuel, thenYO,O=0.232{\displaystyle Y_{O,O}=0.232} andYF,F=1{\displaystyle Y_{F,F}=1}. In addition, assume there is no oxygen in the fuel stream and there is no fuel in the oxidizer stream. Lets{\displaystyle s} be the mass of oxygen required to burn unit mass of fuel (forhydrogen gas,s=8{\displaystyle s=8} and forCmHn{\displaystyle \mathrm {C} _{m}\mathrm {H} _{n}}alkanes,s=32(m+n/4)/(12m+n){\displaystyle s=32(m+n/4)/(12m+n)}[5]). Introduce the scaled mass fractions asyF=YF/YF,F{\displaystyle y_{F}=Y_{F}/Y_{F,F}} andyO=YO/YO,O{\displaystyle y_{O}=Y_{O}/Y_{O,O}}. Then the mixture fraction is defined as

Z=SyFyO+1S+1{\displaystyle Z={\frac {Sy_{F}-y_{O}+1}{S+1}}}

where

S=sYF,FYO,O{\displaystyle S={\frac {sY_{F,F}}{Y_{O,O}}}}

is thestoichiometry parameter, also known as the overallequivalence ratio. On the fuel-stream boundary,yF=1{\displaystyle y_{F}=1} andyO=0{\displaystyle y_{O}=0} since there is no oxygen in the fuel stream, and henceZ=1{\displaystyle Z=1}. Similarly, on the oxidizer-stream boundary,yF=0{\displaystyle y_{F}=0} andyO=1{\displaystyle y_{O}=1} so thatZ=0{\displaystyle Z=0}. Anywhere else in the mixing domain,0<Z<1{\displaystyle 0<Z<1}. The mixture fraction is a function of both the spatial coordinatesx{\displaystyle \mathbf {x} } and the timet{\displaystyle t}, i.e.,Z=Z(x,t).{\displaystyle Z=Z(\mathbf {x} ,t).}

Within the mixing domain, there are level surfaces where fuel and oxygen are found to be mixed in stoichiometric proportion. This surface is special in combustion because this is where a diffusion flame resides. Constant level of this surface is identified from the equationZ(x,t)=Zs{\displaystyle Z(\mathbf {x} ,t)=Z_{s}}, whereZs{\displaystyle Z_{s}} is called as the stoichiometric mixture fraction which is obtained by settingYF=YO=0{\displaystyle Y_{F}=Y_{O}=0} (since if they were react to consume fuel and oxygen, only on the stoichiometric locations both fuel and oxygen will be consumed completely) in the definition ofZ{\displaystyle Z} to obtain

Zs=1S+1{\displaystyle Z_{s}={\frac {1}{S+1}}}.

Relation between local equivalence ratio and mixture fraction

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When there is no chemical reaction, or considering the unburnt side of the flame, the mass fraction of fuel and oxidizer areyF,u=Z{\displaystyle y_{F,u}=Z} andyO,u=1Z{\displaystyle y_{O,u}=1-Z} (the subscriptu{\displaystyle u} denotes unburnt mixture). This allows to define a localfuel-air equivalence ratioϕ{\displaystyle \phi }

ϕ=sYF,uYO,u=SyF,uyO,u.{\displaystyle \phi ={\frac {sY_{F,u}}{Y_{O,u}}}={\frac {Sy_{F,u}}{y_{O,u}}}.}

The local equivalence ratio is an important quantity for partially premixed combustion. The relation between local equivalence ratio and mixture fraction is given by

ϕ=SZ1ZZ=ϕS+ϕ.{\displaystyle \phi ={\frac {SZ}{1-Z}}\qquad \Rightarrow \qquad Z={\frac {\phi }{S+\phi }}.}

The stoichiometric mixture fractionZs{\displaystyle Z_{s}} defined earlier is the location where the local equivalence ratioϕ=1{\displaystyle \phi =1}.

Scalar dissipation rate

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In turbulent combustion, a quantity called the scalar dissipation rateχ{\displaystyle \chi } with dimensional units of that of an inverse time is used to define a characteristic diffusion time. Its definition is given by

χ=2D|Z|2{\displaystyle \chi =2D|\nabla Z|^{2}}

whereD{\displaystyle D} is the diffusion coefficient of the scalar. Its stoichiometric value isχs=2Ds|Z|s2{\displaystyle \chi _{s}=2D_{s}|\nabla Z|_{s}^{2}}.

Liñán's mixture fraction

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Amable Liñán introduced a modified mixture fraction in 1991[6][7] that is appropriate for systems where the fuel and oxidizer have differentLewis numbers. IfLeF{\displaystyle Le_{F}} andLeO2{\displaystyle Le_{O_{2}}} are the Lewis number of the fuel and oxidizer, respectively, then Liñán's mixture fraction is defined as

Z~=S~yFyO+1S~+1{\displaystyle {\tilde {Z}}={\frac {{\tilde {S}}y_{F}-y_{O}+1}{{\tilde {S}}+1}}}

where

S~=LeOSLeF.{\displaystyle {\tilde {S}}={\frac {Le_{O}S}{Le_{F}}}.}

The stoichiometric mixture fractionZ~s{\displaystyle {\tilde {Z}}_{s}} is given by

Z~s=1S~+1{\displaystyle {\tilde {Z}}_{s}={\frac {1}{{\tilde {S}}+1}}}.

References

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  1. ^Williams, F. A. (2018). Combustion theory. CRC Press.
  2. ^Peters, N. (2001). Turbulent combustion.
  3. ^Peters, N. (1992). Fifteen lectures on laminar and turbulent combustion. Ercoftac Summer School, 1428, 245.
  4. ^Liñán, A., & Williams, F. A. (1993). Fundamental aspects of combustion.
  5. ^Fernández-Tarrazo, E., Sánchez, A. L., Linan, A., & Williams, F. A. (2006). A simple one-step chemistry model for partially premixed hydrocarbon combustion. Combustion and Flame, 147(1-2), 32-38.
  6. ^A. Liñán, The structure of diffusion flames, in Fluid Dynamical Aspects of Combustion Theory, M. Onofri and A. Tesei, eds., Harlow, UK. Longman Scientific and Technical, 1991, pp. 11–29
  7. ^Linán, A. (2001). Diffusion-controlled combustion. In Mechanics for a New Mellennium (pp. 487-502). Springer, Dordrecht.
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