Computational Modeling of T5 Laminar and Turbulent Heating Data on Blunt Cones, Part 1: Titan Applications
Author:
Affiliation:
1. NASA Ames Research Center
2. California Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-176
Reference23 articles.
1. Liechty, D.S. and Hollis, B.R. "Heat Shield Cavity Parametric Experimental Aeroheating for a Mars Smart Lander," AIAAPaperNo. 7002-2746,Jun.2002.
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