|Table of Contents|

Review on liquid film cooling of liquid rocket engine(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2020年01期
Page:
1-12
Research Field:
专论与综述
Publishing date:

Info

Title:
Review on liquid film cooling of liquid rocket engine
Author(s):
TANG Liang LI Ping ZHOU Lixin
(Science and Technology on Liquid Rocket Engine Laboratory, Xi’an Aerospace Propulsion Institute, Xi’an 710100, China)
Keywords:
liquid rocket engine liquid film cooling liquid film entrainment heat transfer
PACS:
V434.14文献标识码:A 文章编号:1672-9374(2020)01-0001-12
DOI:
-
Abstract:
Liquid film cooling is an important cooling method for liquid rocket engine.It has the advantages of simple cooling structure and strong cooling capacity.It is generally combined with other cooling methods to achieve the engine cooling.Liquid film cooling has a significant impact on the thermal protection reliability and specific impulse of the liquid rocket engine.In this paper, the research literature on liquid film cooling is reviewed from the aspects of liquid film formation, liquid entrainment, liquid film cooling analysis model and the effect on engine performance.The shortcomings in the current researches are summarized, and the research prospects are proposed from the aspects of the coolant injection structure, the entrainment characteristics of liquid film by the central airflow, the calculation method of liquid film cooling in liquid rocket engine, and the new structure/technical solution of thrust chamber.

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Last Update: 2020-02-25