An Inverse Parameter Estimation Methodology for the Analysis of Aeroheating and Thermal Protection System Experimental Data
Author:
Affiliation:
1. Georgia Institute of Technology
2. ERC, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-4027
Reference26 articles.
1. Afterbody Aeroheating Flight Data for Planetary Probe Thermal Protection System Design
2. Mars Pathfinder Entry Temperature Data, Aerothermal Heating, and Heatshield Material Response
3. A Review of Aerothermal Modeling for Mars Entry Missions
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