Computational Modeling of T5 Laminar and Turbulent Heating Data on Blunt Cones, Part 2: Mars Applications-Reference-Cited by-同舟云学术

Computational Modeling of T5 Laminar and Turbulent Heating Data on Blunt Cones, Part 2: Mars Applications

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Wright Michael¹,Olejniczak Joseph¹,Brown James¹,Hornung Hans²,Edquist Karl³

Affiliation:

1. NASA Ames Research Center

2. California Institute of Technology

3. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-177

Reference47 articles.

1. Martin Marietta Corp."Viking Lander System Primary Mission Performance Report," NASA CR-145148,1977.

2. Edquist, K.T., Liechty, D.S., Hollis, B.R., Alter, S.J., and Loomis, M. "Aeroheating Environments for a Mars SmartLander,"AIAA Paper No. 2002-4505,Aug.2002.

3. Liechty, D.S. and Hollis, B.R. "Heat Shield Parametric Experimental Aeroheating for a Mars Smart Lander," AIAA Paper No. 2002-2746,Jun.2002.

4. Hollis, B.R. and Liechty, D.S. "Boundary Layer Transition Correlations and Aeroheating Predictions for Mars SmartLander,"AIAA Paper No. 2002-2745,Jun.2002.

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