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    Numerical Study of Impingement Cooling of Aviation Kerosene at Supercritical Conditions

    Source: Journal of Heat Transfer:;2018:;volume( 140 ):;issue: 011::page 112201
    Author:
    Xing, Yunfei
    ,
    Zhong, Fengquan
    ,
    Zhang, Xinyu
    DOI: 10.1115/1.4040612
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the present paper, numerical study of flow and heat transfer properties of RP-3 kerosene at liquid and supercritical conditions in an impingement model is conducted with renormalization group (RNG) k−ε turbulence model and a ten-species surrogate of kerosene. The independence of grids is first studied, and the numerical results are compared with experimental data for validation. Characteristics of flow and heat transfer of kerosene flow in the impingement model are studied with different inlet mass flow rates and different inlet temperatures. The velocity and temperature field show similar profile compared to that of air impingement. The heat transfer rates increase first with the increasing of inlet temperature and then decrease suddenly when the inlet temperature is 500 K.
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      Numerical Study of Impingement Cooling of Aviation Kerosene at Supercritical Conditions

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4251875
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    contributor authorXing, Yunfei
    contributor authorZhong, Fengquan
    contributor authorZhang, Xinyu
    date accessioned2019-02-28T11:01:42Z
    date available2019-02-28T11:01:42Z
    date copyright7/23/2018 12:00:00 AM
    date issued2018
    identifier issn0022-1481
    identifier otherht_140_11_112201.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4251875
    description abstractIn the present paper, numerical study of flow and heat transfer properties of RP-3 kerosene at liquid and supercritical conditions in an impingement model is conducted with renormalization group (RNG) k−ε turbulence model and a ten-species surrogate of kerosene. The independence of grids is first studied, and the numerical results are compared with experimental data for validation. Characteristics of flow and heat transfer of kerosene flow in the impingement model are studied with different inlet mass flow rates and different inlet temperatures. The velocity and temperature field show similar profile compared to that of air impingement. The heat transfer rates increase first with the increasing of inlet temperature and then decrease suddenly when the inlet temperature is 500 K.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleNumerical Study of Impingement Cooling of Aviation Kerosene at Supercritical Conditions
    typeJournal Paper
    journal volume140
    journal issue11
    journal titleJournal of Heat Transfer
    identifier doi10.1115/1.4040612
    journal fristpage112201
    journal lastpage112201-7
    treeJournal of Heat Transfer:;2018:;volume( 140 ):;issue: 011
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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