Numerical investigation on flow and convective heat transfer of aviation kerosene at supercritical conditions

	Numerical investigation on flow and convective heat transfer of aviation kerosene at supercritical conditions
	Dang GX(党国鑫); Zhong FQ(仲峰泉); Chen LH(陈立红); Zhang XY(张新宇); Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
发表期刊	SCIENCE CHINA-TECHNOLOGICAL SCIENCES
	2013-02
卷号	56 期号:2 页码:416-422
ISSN	1674-7321
摘要	avier-Stokes equations were solved using RNG k-epsilon turbulence model with low Reynolds number correction. The thermophysical and transport properties of the China RP-3 kerosene were calculated with a 10-species surrogate and the extended corresponding state method (ECS) combined with Benedict-Webb-Rubin equation. The independence of grids was first studied and the numerical results were then compared with experimental data for validation. Under flow conditions given in the paper, the results show that deterioration of convective heat transfer occurs when the wall temperature is slightly higher than the pseudo-critical temperature of kerosene for cases with wall heat flux of 1.2 and 0.8 MW/m(2). The degree of the heat transfer deterioration is weakened as the heat flux decreases. The deterioration, however, does not happen when the heat flux on the pipe wall is reduced to 0.5 MW/m(2). Based on the analysis of the near-wall turbulent properties, it is found that the heat transfer deterioration and then the enhancement are attributed partly to the change in the turbulent kinetic energy in the vicinity of pipe wall. The conventional heat transfer relations such as Sieder-Tate and Gnielinski formulas can be used for the estimation of kerosene heat convection under subcritical conditions, but they are not capable of predicting the phenomenon of heat transfer deterioration. The modified Bae-Kim formula can describe the heat transfer deterioration. In addition, the frictional drag would increase dramatically when the fuel transforms to the supercritical state.
学科领域	流体力学
URL	查看原文
收录类别	SCI ; EI
语种	英语
WOS记录号	WOS:000314913300018
项目资助者	National Natural Science Foundation of China [10921062, 10902115, 11172309]
课题组名称	LHD高超声速推进技术
论文分区	二类/Q2
引用统计	被引频次：23[WOS] [WOS记录] [WOS相关记录]
文献类型	期刊论文
条目标识符	http://dspace.imech.ac.cn/handle/311007/46937
专题	高温气体动力学国家重点实验室
通讯作者	Zhong, FQ (reprint author), 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	Dang GX,Zhong FQ,Chen LH,et al. Numerical investigation on flow and convective heat transfer of aviation kerosene at supercritical conditions[J]. SCIENCE CHINA-TECHNOLOGICAL SCIENCES,2013,56,2,:416-422.
APA	Dang GX,Zhong FQ,Chen LH,Zhang XY,&Zhong, FQ .(2013).Numerical investigation on flow and convective heat transfer of aviation kerosene at supercritical conditions.SCIENCE CHINA-TECHNOLOGICAL SCIENCES,56(2),416-422.
MLA	Dang GX,et al."Numerical investigation on flow and convective heat transfer of aviation kerosene at supercritical conditions".SCIENCE CHINA-TECHNOLOGICAL SCIENCES 56.2(2013):416-422.

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