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    Coupled Heat Transfer Properties of Aluminum/Titanium Alloy Plates With Kerosene Active Cooling

    Source: Journal of Thermal Science and Engineering Applications:;2022:;volume( 014 ):;issue: 009::page 91016-1
    Author:
    Hu, Guohao
    ,
    Zhong, Fengquan
    ,
    Du, Mengmeng
    ,
    Wang, Qinyang
    ,
    Kang, Honglin
    DOI: 10.1115/1.4054009
    Publisher: The American Society of Mechanical Engineers (ASME)
    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/m2. 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 m2 K/W and is 0.015–0.073 m2 K/W for titanium alloy plates. For both materials, conductive thermal resistance dominates the total thermal resistance of plates with active cooling.
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      Coupled Heat Transfer Properties of Aluminum/Titanium Alloy Plates With Kerosene Active Cooling

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4284466
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    contributor authorHu, Guohao
    contributor authorZhong, Fengquan
    contributor authorDu, Mengmeng
    contributor authorWang, Qinyang
    contributor authorKang, Honglin
    date accessioned2022-05-08T08:53:18Z
    date available2022-05-08T08:53:18Z
    date copyright4/6/2022 12:00:00 AM
    date issued2022
    identifier issn1948-5085
    identifier othertsea_14_9_091016.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4284466
    description abstractActive 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/m2. 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 m2 K/W and is 0.015–0.073 m2 K/W for titanium alloy plates. For both materials, conductive thermal resistance dominates the total thermal resistance of plates with active cooling.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleCoupled Heat Transfer Properties of Aluminum/Titanium Alloy Plates With Kerosene Active Cooling
    typeJournal Paper
    journal volume14
    journal issue9
    journal titleJournal of Thermal Science and Engineering Applications
    identifier doi10.1115/1.4054009
    journal fristpage91016-1
    journal lastpage91016-12
    page12
    treeJournal of Thermal Science and Engineering Applications:;2022:;volume( 014 ):;issue: 009
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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