Quantifying the surface heat transfer on transpiration cooled porous materials in laminar and turbulent hypersonic boundary layers
The design of a transpiration cooled system requires detailed local heat transfer information on and in the vicinity of the porous injector; however, limited spatially resolved experimental studies exist, particularly in hypersonic flows. In this work experiments were conducted on a flat plate model...
| Үндсэн зохиолчид: | , , , , , , |
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| Формат: | Conference item |
| Хэл сонгох: | English |
| Хэвлэсэн: |
ESA Conference Bureau / ATPI Corporate Events
2022
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