Effects of Different Structural Film Cooling on Cooling Performance in a GO<sub>2</sub>/GH<sub>2</sub> Subscale Thrust Chamber
To investigate the wall cooling of the thrust chamber in an engine, two film-cooling structures, namely, a circular hole structure and a slot structure, were designed. Numerical simulations were performed to study the coupled flow and regenerative cooling heat transfer in thrust chambers with differ...
| Published in: | Aerospace |
|---|---|
| Main Authors: | , , , |
| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2024-05-01
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| Subjects: | |
| Online Access: | https://www.mdpi.com/2226-4310/11/6/433 |