The Influence of Ablation on Radiative Heating for Earth Entry-Reference-Cited by-同舟云学术

The Influence of Ablation on Radiative Heating for Earth Entry

Published:2008-06-15 Issue: Volume: Page:
ISSN:
Container-title:40th Thermophysics Conference
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Author:

Johnston Christopher¹,Gnoffo Peter¹,Sutton Kenneth²

Affiliation:

1. NASA Langley Research Center

2. National Institute of Aerospace

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-4107

Reference83 articles.

1. Convective and radiative heat transfer to an ablating body.

2. Wilson, K. H., and Hoshizaki, H. "Effect of Ablation Product Absorption and Line Transitions on Shock Layer Radiative Transport,"NASA CR-1264,1969.

3. Radiation transport for stagnation flows including effects of lines and ablation layer.

4. Rigdon, W. S., Dirling, R. B., and Thomas, M. "Stagnation Point Heat Transfer During Hypervelocity Atmospheric Entry," NASA CR-1462,1970.

5. Smith, G. L., Suttles, J. T., Sullivan, E. M., and Graves, R. A. "Viscous Radiating Flowfield on an Ablating Blunt Body," AIAA Paper 70-218,1970.

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