MEDLI2: MISP Inferred Aerothermal Environment and Flow Transition Assessment
Author:
Affiliation:
1. NASA Ames Research Center
2. AMA Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0552
Reference22 articles.
1. Reconstruction of Aerothermal Environment and Heat Shield Response of Mars Science Laboratory
2. Sizing and Margins Assessment of the Mars Science Laboratory Aeroshell Thermal Protection System
3. Development of the Mars Science Laboratory Heatshield Thermal Protection System
4. Discrete-Roughness Transition for Hypersonic Flight Vehicles
5. Flight Experiment Verification of Shuttle Boundary Layer Transition Prediction Tool
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