Fundamental research progress in regenerative cooling for methane engine thrust chambers
文献类型:期刊论文
作者 | Yao Y(姚远)5,6![]() ![]() ![]() |
刊名 | APPLIED THERMAL ENGINEERING
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出版日期 | 2025 |
卷号 | 258页码:16 |
关键词 | Regenerative Cooling Engine Thrust Chambers Transcritical Flow and Heat Transfer Methane Propellant Review |
ISSN号 | 1359-4311 |
DOI | 10.1016/j.applthermaleng.2024.124572 |
通讯作者 | Wei, Xiaolin() |
英文摘要 | Regenerative cooling technologies are recognized as an effective and feasible thermal protection method in liquid oxygen/methane engines. This paper presents a comprehensive review of regenerative cooling applications in engine thrust chambers. The current research on regenerative cooling, including its flow and heat transfer characteristics, is summarized. Additionally, the interrelationships among influential factors, dimensional analysis, transcritical flow and heat transfer mechanisms, as well as heat transfer and pressure drop correlations, are thoroughly examined through numerical simulations and experimental validation. Despite advancements, the cooling capacity of regenerative systems remains insufficient for engines due to the complex operating conditions within thrust chambers and the limited coolant mass flow rate. To mitigate heat transfer deterioration, the paper discusses physical property models, criteria for heat transfer enhancement and deterioration, and predictions based on heat transfer correlations. Furthermore, inconsistencies in descriptions near the pseudo- critical region significantly limit the applicability of existing heat transfer mechanisms and correlations. In light of this, further research is necessary to elucidate heat transfer deterioration mechanisms, cyclic life sensitivity, the combined effects of mini-channel scale and transcritical conditions, and methods to enhance cooling performance. These investigations will lay the groundwork for fundamental research and the development of reusable launch vehicles. |
分类号 | 一类 |
WOS关键词 | CONVECTIVE HEAT-TRANSFER ; SUPERCRITICAL CARBON-DIOXIDE ; PRESSURE-DROP CHARACTERISTICS ; CHEMICAL-VAPOR-DEPOSITION ; TRANSFER DETERIORATION ; NUMERICAL-ANALYSIS ; CRYOGENIC METHANE ; TRANSCRITICAL METHANE ; FORCED-CONVECTION ; FLOW |
资助项目 | National Natural Science Foundation of China[52406118] ; National Natural Science Foundation of China[52322602] ; National Natural Science Foundation of China[52036010] ; State Key Laboratory of Technologies in Space Cryogenic Propellants[SKLTSCP202209] ; Guangxi Key Research and Development Program[AB22035044] ; CAS Key Laboratory of Cryogenics, TIPC[CRYO202103] |
WOS研究方向 | Thermodynamics ; Energy & Fuels ; Engineering ; Mechanics |
语种 | 英语 |
WOS记录号 | WOS:001342329400001 |
资助机构 | National Natural Science Foundation of China ; State Key Laboratory of Technologies in Space Cryogenic Propellants ; Guangxi Key Research and Development Program ; CAS Key Laboratory of Cryogenics, TIPC |
其他责任者 | Wei, Xiaolin |
源URL | [http://dspace.imech.ac.cn/handle/311007/97139] ![]() |
专题 | 力学研究所_高温气体动力学国家重点实验室 |
作者单位 | 1.Tech Inst Phys & Chem, State Key Lab Cryogen Sci & Technol, Beijing 100190, Peoples R China 2.Shanghai Marine Diesel Engine Res Inst, Shanghai 201203, Peoples R China; 3.State Key Lab Technol Space Cryogen Propellants, Beijing 100028, Peoples R China; 4.Univ Chinese Acad Sci, Beijing 100049, Peoples R China; 5.Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China; 6.Beijing Jiaotong Univ, Sch Mech & Elect Engn, Beijing 100044, Peoples R China; |
推荐引用方式 GB/T 7714 | Yao Y,Chen, Qi,Bin F,et al. Fundamental research progress in regenerative cooling for methane engine thrust chambers[J]. APPLIED THERMAL ENGINEERING,2025,258:16. |
APA | 姚远.,Chen, Qi.,宾峰.,Qiu, Yinan.,Yang, Zhiqiang.,...&魏小林.(2025).Fundamental research progress in regenerative cooling for methane engine thrust chambers.APPLIED THERMAL ENGINEERING,258,16. |
MLA | 姚远,et al."Fundamental research progress in regenerative cooling for methane engine thrust chambers".APPLIED THERMAL ENGINEERING 258(2025):16. |
入库方式: OAI收割
来源:力学研究所
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