Advanced Models for Vibrational and Chemical Kinetics Applied to Mars Entry Aerothermodynamics
Author:
Affiliation:
1. Consiglio Nazionale delle Ricerche, 70126 Bari, Italy
2. Ingénierie et Systèmes Avancés, 33700 Mérignac, France
3. St. Petersburg University, 198504, Saint Petersburg, Russia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.T4708
Reference42 articles.
1. Survey of aerodynamics and aerothermodynamics efforts carried out in the frame of Mars exploration projects
2. Modeling of Shock Tunnel Aeroheating Data on the Mars Science Laboratory Aeroshell
3. Influence of Radiative Heating on a Martian Orbiter
4. Time-Dependent Mars Entry Aeroheating Estimation from Simulated In-Depth Heat Shield Temperature Measurements
5. State-to-state models for CO2 molecules: From the theory to an application to hypersonic boundary layers
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