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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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