A Coupled Heat Transfer Calculation Strategy for Composite Cooling Liquid Rocket Engine

To better understand the characteristics of coupled heat transfer in liquid rocket engines, a calculation scheme is proposed in this paper. This scheme can simulate the coupled heat transfer processes, including combustion and flow in the thrust chamber, radiation heat transfer, heat conduction in t...

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Bibliographic Details
Main Authors: Bo Xu, Bing Chen, Jian Peng, Wenyuan Zhou, Xu Xu
Format: Article
Language:English
Published: MDPI AG 2023-05-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/10/5/473