High-Fidelity Charring Ablator Thermal Response Model
Author:
Affiliation:
1. NASA Ames Research Center
2. University of California, Santa Cruz
3. von Kármán Institute for Fluid Dynamics
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3124
Reference14 articles.
1. Overview of the MEDLI Project
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