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contributor authorXing, Yunfei
contributor authorFan, Wenhui
contributor authorDu, Mengmeng
contributor authorZhong, Fengquan
date accessioned2022-05-08T09:26:05Z
date available2022-05-08T09:26:05Z
date copyright4/20/2022 12:00:00 AM
date issued2022
identifier issn0022-1481
identifier otherht_144_07_074501.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4285132
description abstractIn the present paper, numerical study of flow and heat transfer properties of RP-3 kerosene in an impingement model are conducted with SST k−ω turbulence model and a 10-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 temperatures, dimensionless open areas, and separation distances. The heat transfer coefficients and pressure losses increase with decreasing dimensionless open areas. The separation distance H/d = 2 gets the best heat transfer performance and the separation distance H/d = 3 gets the best heat transfer uniformity on the target plate. Higher inlet temperature gets a higher heat transfer performance and heat transfer uniformity on the target plate.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Influence of Geometrical and Inlet Parameters on the Impingement Cooling of Aviation Kerosene
typeJournal Paper
journal volume144
journal issue7
journal titleJournal of Heat Transfer
identifier doi10.1115/1.4054278
journal fristpage74501-1
journal lastpage74501-5
page5
treeJournal of Heat Transfer:;2022:;volume( 144 ):;issue: 007
contenttypeFulltext


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