Strongly Coupled Computation of Material Response and Nonequilibrium Flow for Hypersonic Ablation
Author:
Affiliation:
1. Department of Mechanical Engineering, University of Kentucky, Lexington, Kentucky 40506
2. Department of Aerospace Engineering, University of Michigan, Ann Arbor, Michigan 48109
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A32847
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