A novel heat transfer modeling methodology for regenerative cooling in liquid propellant rocket engines
Liquid propellant rocket engines operate at extremely high temperatures and commonly rely on regenerative cooling to protect chamber walls and maintain structural integrity. Accurate thermal modeling of these systems remains challenging due to the complex heat transfer phenomena, reliance on assumpt...
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| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Elsevier
2025-09-01
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| Series: | Case Studies in Thermal Engineering |
| Subjects: | |
| Online Access: | http://www.sciencedirect.com/science/article/pii/S2214157X25008834 |
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