Coupled radiation effects in thermochemical nonequilibrium shock-capturing flowfield calculations

Author:

Hartung Lin C.1,Mitcheltree Robert A.1,Gnoffo Peter A.1

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering

Cited by 13 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Assessment of Radiative Heating for Hypersonic Earth Reentry Using Nongray Step Models;Aerospace;2022-04-15

2. Flow-radiation coupling for atmospheric entries using a Hybrid Statistical Narrow Band model;Journal of Quantitative Spectroscopy and Radiative Transfer;2016-09

3. Coupled Nonequilibrium Flowfield–Radiative Transfer Calculation Behind a Shock Wave;Journal of Thermophysics and Heat Transfer;2013-07

4. Radiation Phenomena behind Shock Waves;High Temperature Phenomena in Shock Waves;2012

5. Convective and Radiative Heat Flux Estimation on a Reentry Capsule;10th AIAA/ASME Joint Thermophysics and Heat Transfer Conference;2010-06-28

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