Navier-Stokes heating calculations for benchmark thermal protection system sizing
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035-1000
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26842
Reference31 articles.
1. Mars Pathfinder trajectory based heating and ablation calculations
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