Finite-Rate Surface Chemistry Model, II: Coupling to Viscous Navier-Stokes Code
Author:
Affiliation:
1. CUBRC, Inc.
2. SRI International
3. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3784
Reference41 articles.
1. 1Marschall, J. and MacLean, M. "Finite-Rate Surface Chemistry Model, I: Formulation and Reaction System Examples" AIAA Paper Accepted, 42NDThermophysicsConference,Honolulu,HI:27-30June2011.
2. 2Havstad, M. and Ferencz, R. "Comparison of Surface Chemical Kinetic Models for Ablative Reentry of Graphite,"Journal of Thermophysics and Heat Transfer, Vol 16, no 4. Pgs 508 - 515. Oct - Dec 2002.
3. 3Martin, A. and Boyd, I.D. "Implicit Implementation of Material Response and Moving Meshes for Hypersonic Re-entry Ablation," AIAA Paper 2009-0670. 47THAIAAAerospaceSciencesMeeting&Exhibit,Orlando,FL:5-8January2009.
4. 4Johnston, C.O.; Gnoffo, P.A.; and Mazaheri, A. "A Study of Ablation-Flowfield Coupling Relevant to the Orion Heatshield," AIAA Paper 2009-4318. 41STAIAAThermophysicsConference,SanAntonio,TX:22-25June2009.
5. Navier-Stokes Simulations of Hypersonic Flows with Coupled Graphite Ablation
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