Impact of Non-Tangent-Slab Radiative Transport on Flowfield–Radiation Coupling-Reference-Cited by-同舟云学术

Impact of Non-Tangent-Slab Radiative Transport on Flowfield–Radiation Coupling

Published:2018-07 Issue:4 Volume:55 Page:899-913
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Johnston Christopher O.¹,Mazaheri Alireza¹

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A34072

Reference29 articles.

1. Implementation of Radiation, Ablation, and Free Energy Minimization in Hypersonic Simulations

2. JohnstonC. O.GnoffoP. A.MazaheriA. “Influence of Coupled Radiation and Ablation on the Aerothermodynamic Environment of Planetary Entry Vehicles,” VKI Lecture STO-AVT-218, Sint-Genesius-Rode, Belgium, 2013.

3. GnoffoP. A.GuptaR. N.ShinnJ. L. “Conservation Equations and Physical Models for Hypersonic Air Flows in Thermal and Chemical Nonequilibrium,” NASA TP 2867, Feb. 1989.

4. Two-dimensional radiative heat-transfer calculations for nonequilibrium flows

5. Truly two-dimensional algorithms for radiative heat transfer calculations in reactive flows

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