Aerodynamic effects and heat flux augmentation of a transpiration cooled hypersonic sharp leading edge
This paper presents numerical results investigating the aerodynamic and aerothermal effects of mass injection applied to hypersonic sharp leading edges, in the context of active thermal protection systems. A numerical study was carried out using Eilmer to investigate the coupling of leading edge rad...
| Main Authors: | , , , , |
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| Format: | Conference item |
| Language: | English |
| Published: |
American Institute of Aeronautics and Astronautics.
2023
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