A unified methodology for simulation of aerothermochemistry at gas/solid interfaces
Author:
Affiliation:
1. Johns Hopkins Univ., Laurel, MD
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-1086
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4. Nonequilibrium Navier-Stokes Solutions Over an Ablating Graphite Nosetip," J. Spacecraft and Rockets,31,1994.
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2. Parallel Tightly Coupled Solver for Unsteady Hypersonic Ablation of Graphite;40th Fluid Dynamics Conference and Exhibit;2010-06-28
3. High-Fidelity Simulation Strategy for Aerothermochemistry at Ablating Gas/Solid Interfaces;41st Aerospace Sciences Meeting and Exhibit;2003-01-06
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