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)
刊名SCIENCE CHINA-TECHNOLOGICAL SCIENCES
2013-02
通讯作者邮箱fzhong@imech.ac.cn
卷号56期号:2页码:416-422
ISSN号1674-7321
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.
产权排序[Dang GuoXin; Zhong FengQuan; Chen LiHong; Chang XinYu] Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
中文摘要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.
学科主题流体力学
分类号二类/Q2
收录类别SCI ; EI
资助信息National Natural Science Foundation of China [10921062, 10902115, 11172309]
原文出处http://dx.doi.org/10.1007/s11431-012-5075-3
语种英语
WOS记录号WOS:000314913300018
公开日期2013-03-04
内容类型期刊论文
源URL[http://dspace.imech.ac.cn/handle/311007/46937]  
专题力学研究所_高温气体动力学国家重点实验室
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.(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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