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Numerical Heat Transfer, Part A: Applications
An International Journal of Computation and Methodology
Volume 69, 2016 - Issue 2
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Original Articles

Comparative study of thermal radiation properties models in turbulent non-premixed sooting combustion

, &
Pages 166-179 | Received 03 Dec 2014, Accepted 17 Apr 2015, Published online: 23 Sep 2015
 

ABSTRACT

This work presents a numerical study of radiation heat transfer and its interaction with gray and spectral radiation of combustion products and soot that are formed in a turbulent non-premixed combustion process. To this purpose, weighted sum of gray gases (WSGGM), Rayleigh, narrow-band model, and semi-empirical radiation properties models are considered. Two situations are studied −1-D radiation problem and non-premixed gaseous combustion process. The results demonstrate that the models exhibit discrepancies that are smaller than the available line-by-line or experimental data. A study of the factors that influence such a disagreement is presented, underscoring the role of the chemical kinetics of hydrocarbon species and soot oxidation.

Nomenclature

Latin letters=
a=

Global absorption coefficient of the medium

aE=

Mean absorption-emission coefficient

ag=

Gray absorption coefficient of the gaseous medium

asoot=

Gray absorption coefficient of soot

aλ=

Spectral absorption coefficient of the medium

aλ,g=

Spectral absorption coefficient of the gaseous medium

aλ,soot=

Spectral absorption coefficient of soot

dP=

Soot diameter

fV=

Soot volume fraction

It=

Turbulent intensity

lt=

Integral length-scale of turbulence

m=

Complex refractive index

n=

Refractive index

pexit=

Outlet pressure

=

Vector of radiant heat flux

qR=

Magnitude of radiant heat flux

=

Vector position

=

Vector position

=

Vector position

=

Velocity fluctuation

Coxid=

Oxidation scaling parameter of the Moss-Brookes soot model

=

Equivalent soot volume fraction

G=

Incident radiation

I=

Gray intensity of radiant energy

Iλ=

Spectral intensity of radiant energy

Iλ, b=

Spectral intensity of radiant energy emitted by a blackbody

L=

Separation between plates

Lm=

Mean path length

=

Radiation heat transfer rate

=

Total heat transfer rate

Re=

Reynolds number

T=

Temperature of the medium

T0=

Inlet temperature

Texit=

Outlet temperature

Tp=

Wall temperature

Uz, 0=

Inlet velocity at longitudinal direction

XC3H8=

Propane molar fraction

XO2=

Oxygen molar fraction

XN2=

Nitrogen molar fraction

=

Mean mixture fraction

=

Variance of the mixture fraction

Greek letters=
ϵp=

Wall emissivity

λ=

Wavelength

σ=

Stefan-Boltzman constant = 5.67 × 10−8 W/m2 K4

σs=

Gray scattering coefficient of the medium

σs,λ=

Spectral scattering coefficient of the medium

τλ=

Spectral transmissivity

Φ=

Scattering phase function

=

Solid angle

Nomenclature

Latin letters=
a=

Global absorption coefficient of the medium

aE=

Mean absorption-emission coefficient

ag=

Gray absorption coefficient of the gaseous medium

asoot=

Gray absorption coefficient of soot

aλ=

Spectral absorption coefficient of the medium

aλ,g=

Spectral absorption coefficient of the gaseous medium

aλ,soot=

Spectral absorption coefficient of soot

dP=

Soot diameter

fV=

Soot volume fraction

It=

Turbulent intensity

lt=

Integral length-scale of turbulence

m=

Complex refractive index

n=

Refractive index

pexit=

Outlet pressure

=

Vector of radiant heat flux

qR=

Magnitude of radiant heat flux

=

Vector position

=

Vector position

=

Vector position

=

Velocity fluctuation

Coxid=

Oxidation scaling parameter of the Moss-Brookes soot model

=

Equivalent soot volume fraction

G=

Incident radiation

I=

Gray intensity of radiant energy

Iλ=

Spectral intensity of radiant energy

Iλ, b=

Spectral intensity of radiant energy emitted by a blackbody

L=

Separation between plates

Lm=

Mean path length

=

Radiation heat transfer rate

=

Total heat transfer rate

Re=

Reynolds number

T=

Temperature of the medium

T0=

Inlet temperature

Texit=

Outlet temperature

Tp=

Wall temperature

Uz, 0=

Inlet velocity at longitudinal direction

XC3H8=

Propane molar fraction

XO2=

Oxygen molar fraction

XN2=

Nitrogen molar fraction

=

Mean mixture fraction

=

Variance of the mixture fraction

Greek letters=
ϵp=

Wall emissivity

λ=

Wavelength

σ=

Stefan-Boltzman constant = 5.67 × 10−8 W/m2 K4

σs=

Gray scattering coefficient of the medium

σs,λ=

Spectral scattering coefficient of the medium

τλ=

Spectral transmissivity

Φ=

Scattering phase function

=

Solid angle

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