Numerical Study of Spallation Phenomenon in an Arc-Jet Environment
Analyses of thermal protection system response to atmospheric entry are generally performed in a decoupled manner where some terms in
...Modeling of Heat Transfer Attenuation by Ablative Gases During the Stardust Reentry
High performance modeling of atmospheric re-entry vehicles
Computational Fluid Dynamics Analysis of the Kentucky Re-Entry Universal Payload System
The current design of NASA’s Multi-Purpose Crew vehicle uses the latest iteration of AVCOAT, an ablating thermal protection material
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