Influence of helix angle on heat transfer characteristics of regenerative cooling in spiral channel-Reference-Cited by-同舟云学术

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Influence of helix angle on heat transfer characteristics of regenerative cooling in spiral channel

Published:2024-02 Issue: Volume:54 Page:104026
ISSN:2214-157X
Container-title:Case Studies in Thermal Engineering
language:en
Short-container-title:Case Studies in Thermal Engineering

Author:

Liu Xinlin^ORCID,Jiang Zhuohang,Li Qinglian,Song Jie,Cheng Peng

Publisher

Elsevier BV

Reference46 articles.

1. System scheme design for LOX/LCH4 variable thrust liquid rocket engines using motor pump;Cui;Acta Astronaut.,2020

2. Numerical study on the combustion characteristics of a fuel-centered pintle injector for methane rocket engines;Son;Acta Astronaut.,2017

3. System scheme and thermal performance of a third fluid cooled rocket engine;Song;Acta Astronaut.,2022

4. System scheme design of electric expander cycle for LOX/LCH4 variable thrust liquid rocket engine;Liang;Acta Astronaut.,2021

5. Thermal-structural analysis of regeneratively cooled thrust chamber wall in reusable LOX/Methane rocket engines;Song;Chin. J. Aeronaut.,2017

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