A system-level multi-field coupling algorithm for regenerative cooling thrust chamber of a LOX/methane rocket engine-Reference-Cited by-同舟云学术

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A system-level multi-field coupling algorithm for regenerative cooling thrust chamber of a LOX/methane rocket engine

Published:2023-12 Issue: Volume:213 Page:588-602
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Yan Zelong^ORCID,Chen Yang^ORCID,Wu Youliang,Liu Ziyan,Gao Yushan,Wang Weizong

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference57 articles.

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

2. Numerical investigation on the performance of internal flow and atomization in the recessed gas-centered swirl coaxial injectors;Liu;Aero. Sci. Technol.,2022

3. On the characterization of methane in rocket nozzle cooling channels;Heldens;Acta Astronaut.,2021

4. Chemical modeling for methane oxy-combustion in liquid rocket engines;Blanchard;Acta Astronaut.,2022

5. Reusable launch vehicle technology program;Freeman;Acta Astronaut.,1997

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