Numerical Investigation on Transient Heat Transfer of Different Coolants in the Cooling Channel of a Thrust Chamber
Controlling the nozzle wall temperature using regenerative cooling is a highly effective approach in liquid rocket engines. The selection of coolant is critical to determining the cooling system's thermal performance. In this study, the transient and steady-state heat transfer characteristics of a r...
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| Principais autores: | , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
Semnan University
2026-06-01
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| coleção: | Journal of Heat and Mass Transfer Research |
| Assuntos: | |
| Acesso em linha: | https://jhmtr.semnan.ac.ir/article_10532_968b94de47e2612410484039bbc426bb.pdf |
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