Fully-Coupled Simulation of Low Temperature Ablator and Hypersonic Flow Solver
Author:
Affiliation:
1. University of Kentucky College of Engineering
2. University of Maryland at College Park
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0676
Reference45 articles.
1. Space Resource. Ablative materials for high-temperature thermal protection of space vehicles
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3. Fluid-Structure Interactions with Geometrically Nonlinear Deformations
4. A Numerical Investigation of Parachute Deployment in Supersonic Flow
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