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Coupled Heat Transfer Properties of Aluminum/Titanium Alloy Plates With Kerosene Active Cooling
Hu GH(胡国豪)1,2; Zhong FQ(仲峰泉)1,2; Du MM(杜蒙蒙)1,2; Wang, Qinyang3; Kang, Honglin3
通讯作者Zhong, Fengquan(fzhong@imech.ac.cn)
发表期刊JOURNAL OF THERMAL SCIENCE AND ENGINEERING APPLICATIONS
2022-09-01
卷号14期号:9页码:12
ISSN1948-5085
摘要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.
关键词thermal protection active cooling thermal resistance aerospace heat transfer
DOI10.1115/1.4054009
收录类别SCI ; EI
语种英语
WOS记录号WOS:000835413500012
关键词[WOS]SUPERCRITICAL-PRESSURE ; NUMERICAL-ANALYSIS ; AVIATION KEROSENE ; HYDROCARBON FUEL ; SYSTEM ; FLOW
WOS研究方向Thermodynamics ; Engineering
WOS类目Thermodynamics ; Engineering, Mechanical
论文分区Q4
力学所作者排名1
RpAuthorZhong, Fengquan
引用统计
被引频次:1[WOS]   [WOS记录]     [WOS相关记录]
文献类型期刊论文
条目标识符http://dspace.imech.ac.cn/handle/311007/89832
专题高温气体动力学国家重点实验室
作者单位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
推荐引用方式
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.
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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