The Impact of Flowfield-Radiation Coupling on Aeroheating for Titan Aerocapture-Reference-Cited by-同舟云学术

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The Impact of Flowfield-Radiation Coupling on Aeroheating for Titan Aerocapture

Published:2004-01-05 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Wright Michael¹,Prabhu Dinesh¹,Olejniczak Joe²

Affiliation:

1. ELORET Corp.

2. NASA Ames

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-484

Reference14 articles.

1. Mission,"AIAAPaperNo. 2003-4951,Jul.2003. '-Justus, C. and Duvall, A. "Engineering Level Model

2. 2003-4803,Jul.2003.Wright,M.J., Candler,G.V., and Bose, D. "Data-Parallel

3. 17,No. 2,2003,pp.240-249. I' MacCormack,R.W. and Candler, G.V. "The Solution of

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5. Three-Dimensional Radiative Heating of Descent Space Vehicle Based on Spherical Harmonics Method with Unstructured Grids;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09

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