Enhancement of Film Cooling Effectiveness in a Supersonic Nozzle
Film cooling as applied to rocket nozzles is analyzed numerically with emphasis on the assessment of the effect of the mixing of coolant with the hot stream. Cooling performance, as characterized by cooling effectiveness, is studied for three different coolants in the three-dimensional, turbulent fl...
| Main Authors: | , , , , , |
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| Formato: | Artigo |
| Idioma: | English |
| Publicado: |
MDPI AG
2023-03-01
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| Series: | Entropy |
| Subjects: | |
| Acceso en liña: | https://www.mdpi.com/1099-4300/25/3/481 |