Numerical study on flow and heat transfer of aviation kerosene at supercritical pressure in cooling channels with surface corrugations

doi:10.1016/j.icheatmasstransfer.2022.106526

CORC > 力学研究所 > 中国科学院力学研究所 > 高温气体动力学国家重点实验室

	Numerical study on flow and heat transfer of aviation kerosene at supercritical pressure in cooling channels with surface corrugations
	Gao, Erkang 1,2; Fan, Wenhui 1,2; Li, Xian 1,2; Zhong, Fengquan 1,2
刊名	INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER
	2023
卷号	140 页码:14
关键词	Aviation kerosene Surface corrugation Convective heat transfer Supercritical conditions
ISSN号	0735-1933
DOI	10.1016/j.icheatmasstransfer.2022.106526
通讯作者	Zhong, Fengquan(fzhong@imech.ac.cn)
英文摘要	In this paper, turbulent flow of aviation kerosene at supercritical pressure through cooling channels respectively with streamwise sinusoidal corrugation, spanwise sinusoidal corrugation and streamwise and spanwise coupled sinusoidal corrugations are numerically studied. The Reynolds-averaged Navier-Stokes method with RNG k -epsilon turbulence model is used to perform numerical simulation. The independence of grids is first examined, and the numerical results are compared with experimental data for validation. The present results show that the streamwise corrugation significantly improves convective heat transfer performance of cooling channels, the increase ratio of Nusselt number and Thermal Performance Factor reaches 20.44% and 6.7%. With the streamwise and spanwise corrugations coupling, the increase ratio of Nusselt number and Thermal Performance Factor are both larger than those in cooling channels with only streamwise corrugation. Furthermore, the results of flow and heat transfer of aviation kerosene at supercritical conditions with corrugations effect show that corrugations can eliminate heat transfer deterioration occurring at supercritical conditions. The present study is aimed to provide useful references for cooling optimization with wall microstructures for engineering applications.
资助项目	National Natural Science Foundation of China ; [12072351]
WOS关键词	TRANSFER DETERIORATION ; HYDROCARBON FUEL ; HYDRAULIC PERFORMANCE ; EXCHANGER ; RESISTANCE ; PASSAGES ; DROP ; RP-3
WOS研究方向	Thermodynamics ; Mechanics
语种	英语
WOS记录号	WOS:000906920600004
资助机构	National Natural Science Foundation of China
内容类型	期刊论文
源URL	[http://dspace.imech.ac.cn/handle/311007/91445]
专题	力学研究所_高温气体动力学国家重点实验室
通讯作者	Zhong, Fengquan
作者单位	1.Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China 2.Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
推荐引用方式 GB/T 7714	Gao, Erkang,Fan, Wenhui,Li, Xian,et al. Numerical study on flow and heat transfer of aviation kerosene at supercritical pressure in cooling channels with surface corrugations[J]. INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER,2023,140:14.
APA	Gao, Erkang,Fan, Wenhui,Li, Xian,&Zhong, Fengquan.(2023).Numerical study on flow and heat transfer of aviation kerosene at supercritical pressure in cooling channels with surface corrugations.INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER,140,14.
MLA	Gao, Erkang,et al."Numerical study on flow and heat transfer of aviation kerosene at supercritical pressure in cooling channels with surface corrugations".INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER 140(2023):14.