1. School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 15001, China 2. College of Metallurgy and Energy, North China University of Science and Technology, Tangshan 063009, China
This paper investigated radiation heat transfer and temperature distributions of solar thermochemical reactor for syngas production using the finite volume discrete ordinate method (fvDOM) and P1 approximation for radiation heat transfer. Different parameters including absorptivity, emissivity, reflection based radiation scattering, and carrier gas flow inlet velocity that would greatly affect the reactor thermal performance were sufficiently investigated. The fvDOM approximation was used to obtain the radiation intensity distribution along the reactor. The drop in the temperature resulted from the radiation scattering was further investigated using the P1 approximation. The results indicated that the reactor temperature difference between the P1 approximation and the fvDOM radiation model was very close under different operating conditions. However, a big temperature difference which increased with an increase in the radiation emissivity due to the thermal non-equilibrium was observed in the radiation inlet region. It was found that the incident radiation flux distribution had a strong impact on the temperature distribution throughout the reactor. This paper revealed that the temperature drop caused by the boundary radiation heat loss should not be neglected for the thermal performance analysis of solar thermochemical reactor.
Radiation inlet: T = Parameter study Carrier gas inlet: T = 300
300
300
U/(m?s–1)
Fixed value Carrier gas inlet: v = Parameter study Radiation inlet: u = Parameter study
Zero gradient
Zero gradient
Prgh/atm
Fixed flux pressure Value: Parameter study
Zero gradient
Fixed flux pressure Value: Parameter study
P/atm
Calculated Value: internal field
Calculated Value= internal field
Calculated Value: internal field
G/(W?m–2)
Marshak radiation T = Parameter study Emissivity= 1.0 Value: 0.0
Marshak radiation T = Parameter study Emissivity= 1.0 Value: 0.0
Marshak radiation T = Parameter study Emissivity= 1.0 Value: 0.0
I/(W?m–2?sr–1)
Grey diffuse radiation
Grey diffuse radiation
Grey diffuse radiation
aeff/(m2?s–1)
Alphat wall function Value: 0.0
Alphat wall function Value: 0.0
Alphat wall function Value: 0.0
meff/(kg?m–1?s–1)
Mutk wall function Value: 0.00
Mutk wall function Value: 0.00
Mutk wall function Value: 0.00
εT/(m2?s–3)
Epsilon wall function Value: 0.01
Epsilon wall function Value: 0.01
Epsilon wall function Value: 0.01
K/(m2?s–2)
kqR wall function Value: 0.1
kqR wall function Value: 0.1
kqR wall function Value: 0.1
Tab.1
Fig.2
Fig.3
Fig.4
Fig.5
Fig.6
Fig.7
Fig.8
Fig.9
C
Linear anisotropic phase function coefficient
cP
Specific heat capacity at constant pressure, J/(kg?K)
DP
Pressure diffusivity
G
Incident radiation flux, W/m2
Gw
incident radiation flux at the wall, W/m2
g
Gravitational acceleration, m/s2
h
Specific enthalpy, J/kg
Ib,r
Blackbody radiation intensity, W/(m2?mm?sr)
Ir,s
Radiation intensity, W/(m2?sr)
K
Kinetic energy, m2/s2
k
Thermal conductivity, W/(m?K)
Unit normal vector to the wall
P
Total pressure, atm
Pr
Prandtl number
Reference pressure, atm
Prgh
Dynamic pressure, atm
qr
Radiative flux vector, W/m2
r
Point
s
Direction
Sf
Patch face area vectors
T
Temperature, K
Tw
Wall temperature, K
u
Velocity, m/s
Greek letters
α
Absorptivity
αeff
Effective thermal diffusivity, m2/s
εT
Thermal dissipation rate, m2/s3
ε
Emission coefficient
εw
Wall emissivity
ϕ
Flux
Predicted flux field
Absorption coefficient, m-1
μeff
Molecular viscosity, kg/m?s
μ
Dynamic viscosity, kg/m?s
Scattering phase function
ρ
Density, kg/m3
σ
Stefan-Boltzmann constant, W/(m2?K4)
σs
Scattering coefficient
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