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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Bibliographic Details
Main Authors: Volodymyr Sliusariev, Valerii Bucharskyi
Format: Article
Language:English
Published: Oles Honchar Dnipro National University 2024-11-01
Series:Challenges and Issues of Modern Science
Subjects:
Online Access:https://cims.fti.dp.ua/j/article/view/234
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