Details of Modeling Titan Entry Nonequilibrium Radiation with a Multi-Quantum Vibration State CR Model
Author:
Affiliation:
1. Stanford University
2. von Kármán Institute for Fluid Dynamics
3. École Centrale Paris
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4526
Reference24 articles.
1. Nonequilibrium radiative heat flux modeling for the Huygens entry probe
2. A Code Calibration Study for Huygens Entry Aeroheating
3. An Analysis of the Radiative Heating Environment for Aerocapture at Titan
4. Radiaitve Heating Methodology for the Huygens Probe
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