Boundary Layer Stability Analysis of Mars Science Laboratory Aeroshell-Reference-Cited by-同舟云学术

Boundary Layer Stability Analysis of Mars Science Laboratory Aeroshell

Published:2006-01-09 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Johnson Heath¹,Candler Graham¹,Wright Michael²

Affiliation:

1. University of Minnesota

2. NASA Ames Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-920

Reference29 articles.

1. M.J. Wright, J. Olejniczak, J.L. Brown, H.G. Hornung, and K.T. Edquist. “Computational Modeling of T5 Laminar and Turbulent Heating Data on Blunt Cones, Part 2: Mars Applications”. AIAA Paper No. 2005-0177, January 2005.

2. K. T. Edquist, D. S. Liechty, B. R. Hollis, S. J. Alter, and M. Loomis. “Aeroheating Environments for a Mars Smart Lander”. AIAA Paper No. 2002-4505, August 2002.

3. B.R. Hollis, D.S. Liechty, M.J. Wright, M.S. Holden, T.P. Wadhams, M. MacLean, and A. Dyakonov. “Transition Onset and Turbulent Heating Measurements for the Mars Science Laboratory Entry Vehicle”. AIAA Paper No. 2005-1437, January 2005.

4. Algebraic correlations for high-speed transition prediction on sharp and blunt cones

5. M. J. Wright, G. V. Candler, and D. Bose. “A Data-Parallel Line-Relaxation Method for the Navier-Stokes Equations”. AIAA Paper No. 97-2046CP, June 1997.

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