Assessment of Radiative Heating Uncertainty for Hyperbolic Earth Entry
Author:
Affiliation:
1. NASA Langley Research Center
2. NASA Ames Research Center
3. ERC, Inc.
4. University of California Santa Cruz
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3145
Reference178 articles.
1. Entry Trajectory and Aeroheating Environment Definition for Capsule-Shaped Vehicles
2. Convective and radiative heat transfer to an ablating body.
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