Numerical simulation of transpiration cooling with a two-dimensional substructure
This paper presents a numerical model which assesses the coupled effect when transpiration cooling is applied to the external skin of a thermal protection system and the substructure of a high speed flight vehicle. The PIRATE transpiration cooling code has been extended and validated to account for...
| Автори: | , , |
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| Формат: | Conference item |
| Мова: | English |
| Опубліковано: |
ESA Conference Bureau
2019
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