Mathematical model for heat transfer in variable thickness fins for rocket engines
Purpose. This article aims to develop a mathematical model for a fin in the cooling system of liquid propellant rocket engines. The objective is to enable calculations for fins with arbitrary thickness variation. The developed mathematical model will be valuable and in demand for calculating heat t...
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Main Authors: | Volodymyr Sliusariev, Valerii Bucharskyi |
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Format: | Article |
Language: | English |
Published: |
Oles Honchar Dnipro National University
2024-11-01
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Series: | Challenges and Issues of Modern Science |
Subjects: | |
Online Access: | https://cims.fti.dp.ua/j/article/view/234 |
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