Nonequilibrium Finite-Rate Carbon Ablation Model for Earth Reentry Flows
Author:
Affiliation:
1. Air Force Institute of Technology, Wright–Patterson Air Force Base, Ohio 45433
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.A33399
Reference18 articles.
1. Effects of atomic oxygen on graphite ablation
2. Stagnation-point ablation of carbonaceous flat disks. I Theory
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4. Stagnation-Point Heat Transfer Rates for Pioneer-Venus Probes
5. Viscous Shock-Layer Simulation of Airflow past Ablating Blunt Body with Carbon Surface
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