2000
DOI: 10.1016/s0017-9310(99)00384-1
|View full text |Cite
|
Sign up to set email alerts
|

Radiative transfer in arbitrarily-shaped axisymmetric enclosures with anisotropic scattering media

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1

Citation Types

2
6
0
1

Year Published

2004
2004
2019
2019

Publication Types

Select...
5
2

Relationship

0
7

Authors

Journals

citations
Cited by 17 publications
(9 citation statements)
references
References 13 publications
2
6
0
1
Order By: Relevance
“…The geometry of the rocket nozzle model is depicted in Fig.8. The axial temperature distributions of nozzle wall and combustion products are listed in the paper of Nunes et al (2000). The nozzle wall is gray with the emissivity of 0.8; the top boundary of the combustion chamber perpendicular to the x-axis is set to be black with the same temperature of the neighboring gas; the exiting cross-section is assumed to be gray with the emissivity of 0.8 and the temperature equal to the adjacent gas.…”
Section: Rocket Nozzlementioning
confidence: 99%
See 1 more Smart Citation
“…The geometry of the rocket nozzle model is depicted in Fig.8. The axial temperature distributions of nozzle wall and combustion products are listed in the paper of Nunes et al (2000). The nozzle wall is gray with the emissivity of 0.8; the top boundary of the combustion chamber perpendicular to the x-axis is set to be black with the same temperature of the neighboring gas; the exiting cross-section is assumed to be gray with the emissivity of 0.8 and the temperature equal to the adjacent gas.…”
Section: Rocket Nozzlementioning
confidence: 99%
“…The combustion products are treated as the absorbing, emitting and anisotropically scattering soot/carbon particles with the uniform diameter of 30 μm and concentration N p = 5 × 10 8 par/m 3 . The radiation properties of particles are calculated by the expressions of Nunes et al (2000). Figure 9 illustrates the nondimensional radiative heat flux distribution along the nozzle wall.…”
Section: Rocket Nozzlementioning
confidence: 99%
“…As may be surmised from its name, this dimensionless parameter is a measure of the relative importance of conductive heat transfer with respect to radiant transport in an optically thick medium. A reasonable approach for representing internal radiation transport through such materials is called the band approximation, where the medium is assumed to exhibit a combination of transparent and opaque behaviors [79][80][81][82][83][84][85]. Therefore, a better approach is the P 1 approximation, also known as the differential and Milne-Eddington approximations [26], where a finite set of moments are employed to reduce the integral terms of the radiation transfer equation to differential terms.…”
Section: Internal Radiationmentioning
confidence: 99%
“…Using Eqs. (20)(21)(22) and the area elements from Table 1, Eq. (12) yields the following expression: Equations (13) and (14) are similarly treated to yield…”
Section: Problem Statement and Numerical Solution Techniquementioning
confidence: 99%
“…A three-dimensional control volume finite element method for the treatment of the RTE applied to emitting, absorbing, and scattering media was developed by Grissa et al [19]. Two numerical models for solving thermal radiative transport in irregularly shaped axisymmetric geometry containing homogeneous, anisotropically scattering media were presented by Nunes et al [20].…”
mentioning
confidence: 99%