Coupled Heat Transfer Properties of Aluminum/Titanium Alloy Plates With Kerosene Active Cooling | |
Hu GH(胡国豪)1,2![]() ![]() | |
Corresponding Author | Zhong, Fengquan([email protected]) |
Source Publication | JOURNAL OF THERMAL SCIENCE AND ENGINEERING APPLICATIONS
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2022-09-01 | |
Volume | 14Issue:9Pages:12 |
ISSN | 1948-5085 |
Abstract | Active cooling is an effective thermal protection method for plates under high thermal loading. In this paper, characteristics of coupled heat transfer of aluminum alloy and titanium alloy plates with kerosene active cooling are studied numerically and experimentally. The effects of cooling channel spacing as well as the inlet parameters of kerosene on the maximum temperature and temperature uniformity of the plate are investigated with varied heat fluxes. Besides, the thermal resistance and flow resistance of kerosene cooling are also analyzed. The experimental results show that the 2a12-type aluminum alloy plate can be cooled to a maximum temperature of 460 K with kerosene cooling under a mass flowrate of 24.7 g/s and heat flux of 6-11 kW/m(2). The numerical results show that the maximum temperature is mainly affected by the channel spacing and heat flux. Compared to the titanium alloy plate, the aluminum alloy plate is more likely to be affected by the coolant mass flowrate. In addition, the conductive thermal resistance of aluminum alloy plates is 0.0017-0.0079 m(2) K/W and is 0.015-0.073 m(2) K/W for titanium alloy plates. For both materials, conductive thermal resistance dominates the total thermal resistance of plates with active cooling. |
Keyword | thermal protection active cooling thermal resistance aerospace heat transfer |
DOI | 10.1115/1.4054009 |
Indexed By | SCI ; EI |
Language | 英语 |
WOS ID | WOS:000835413500012 |
WOS Keyword | SUPERCRITICAL-PRESSURE ; NUMERICAL-ANALYSIS ; AVIATION KEROSENE ; HYDROCARBON FUEL ; SYSTEM ; FLOW |
WOS Research Area | Thermodynamics ; Engineering |
WOS Subject | Thermodynamics ; Engineering, Mechanical |
Classification | Q4 |
Ranking | 1 |
Contributor | Zhong, Fengquan |
Citation statistics | |
Document Type | 期刊论文 |
Identifier | http://dspace.imech.ac.cn/handle/311007/89832 |
Collection | 高温气体动力学国家重点实验室 |
Affiliation | 1.Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China; 2.Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China; 3.Beijing Aerosp Technol Inst, Beijing 100074, Peoples R China |
Recommended Citation GB/T 7714 | Hu GH,Zhong FQ,Du MM,et al. Coupled Heat Transfer Properties of Aluminum/Titanium Alloy Plates With Kerosene Active Cooling[J]. JOURNAL OF THERMAL SCIENCE AND ENGINEERING APPLICATIONS,2022,14,9,:12.Rp_Au:Zhong, Fengquan |
APA | 胡国豪,仲峰泉,杜蒙蒙,Wang, Qinyang,&Kang, Honglin.(2022).Coupled Heat Transfer Properties of Aluminum/Titanium Alloy Plates With Kerosene Active Cooling.JOURNAL OF THERMAL SCIENCE AND ENGINEERING APPLICATIONS,14(9),12. |
MLA | 胡国豪,et al."Coupled Heat Transfer Properties of Aluminum/Titanium Alloy Plates With Kerosene Active Cooling".JOURNAL OF THERMAL SCIENCE AND ENGINEERING APPLICATIONS 14.9(2022):12. |
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