Influence of Ablation Products on the Radiation at the Surface of a Blunt Hypersonic Vehicle at 10 km/s

Author:

Laux Christophe1,Winter Michael1,Merrifield James2,Smith Arthur2,Tran Philippe3

Affiliation:

1. École Centrale Paris

2. Fluid Gravity Engineering Ltd

3. Astrium-ST

Publisher

American Institute of Aeronautics and Astronautics

Reference13 articles.

1. 1NetterfieldM.P.,ValidationofaNavier-StokesCodeforThermochemicalNon-EquilibriumFlows,AIAA92-2878

2. Evaluation of Real-Gas Phenomena in High-Enthalpy Aerothermal Test Facilities: A Review

3. 4Park,C."ReviewofChemical-KineticProblemsofFutureNASAMissions,I:EarthEntries,"JournalofThermophysics and HeatTransfer,Volume7,No.3,pp.385-398,1993.

4. 5Knab, O., Frühauf, H.H. and Messerschmid, E. W.: Validation of a Physically Consistent Coupled Vibration-Chemistry-Vibration Model for Ionized Airin Thermo-ChemicalNonequilibrium,AIAA-Paper93-2866,1993.

5. 6Blottner, F.G, Johnson, M., Ellis, M., Chemically reacting viscous flow program for multi-component gas mixtures, Sandia Laboratories,Albuquerque,New Mexico,Report SC-RR-70-754,1971.

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