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CLC number: TK124

On-line Access: 2018-02-05

Received: 2016-03-28

Revision Accepted: 2016-07-18

Crosschecked: 2018-01-16

Cited: 0

Clicked: 12427

Citations:  Bibtex RefMan EndNote GB/T7714

 ORCID:

Wei Li

https://orcid.org/0000-0002-2295-2542

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Journal of Zhejiang University SCIENCE A 2018 Vol.19 No.2 P.158-170

10.1631/jzus.A1600276


Numerical study of heat transfer characteristics of downward supercritical kerosene flow inside circular tubes


Author(s):  Jing-zhi Zhang, Jin-pin Lin, Dan Huang, Wei Li

Affiliation(s):  Department of Energy Engineering, Zhejiang University, Hangzhou 310027, China; more

Corresponding email(s):   weili96@zju.edu.cn

Key Words:  Aviation kerosene, Heat transfer deterioration, Supercritical pressure, Numerical study


Jing-zhi Zhang, Jin-pin Lin, Dan Huang, Wei Li. Numerical study of heat transfer characteristics of downward supercritical kerosene flow inside circular tubes[J]. Journal of Zhejiang University Science A, 2018, 19(2): 158-170.

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T1 - Numerical study of heat transfer characteristics of downward supercritical kerosene flow inside circular tubes
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DOI - 10.1631/jzus.A1600276


Abstract: 
The heat transfer characteristics of China RP-3 aviation kerosene flowing in a vertical downward tube with an inner diameter of 4 mm under supercritical pressures are numerically studied. A ten-species surrogate model is used to calculate the thermophysical properties of kerosene and the re-normalization group (RNG) k-ε turbulent model with the enhanced wall treatment is adopted to consider the turbulent effect. The effects of mass flow rate, wall heat flux, inlet temperature, and pressure on heat transfer are investigated. The numerical results show that three types of heat transfer deterioration exist for the aviation kerosene flow. The first type of deterioration occurred at the tube inlet region and is caused by the development of the thermal boundary layer, while the other two types are observed when the inner wall temperature or the bulk fuel temperature approaches the pseudo-critical temperature. The heat transfer coefficient increases with the increasing mass flow rate and the decreasing wall heat flux, while the inlet bulk fluid temperature only influences the starting point of the heat transfer coefficient curve plotted against the bulk fluid temperature. The increase of inlet pressure can effectively eliminate the deterioration due to the small variations of properties near the pseudo-critical point at relatively high pressure. The numerical heat transfer coefficients fit well with the empirical correlations, especially at higher pressures (about 5 MPa).

圆管内向下流超临界航空煤油换热特性数值研究

目的:超临界航空煤油在换热过程中会出现传热恶化的现象.本文旨在研究该现象产生的原因及质量流量、壁面热流、入口温度和压力对此现象的影响.
创新点:1. 分析超临界航空煤油的传热恶化现象; 2. 揭示超临界航空煤油传热过程中传热恶化现象与质量流量、壁面热流、入口温度及压力的关系.
方法:利用数值模拟的方法,模拟超临界航空煤油在管内的流动换热情况,分析其换热特性,并探讨传热恶化产生的原因及影响因素.
结论:1. 传热恶化是在壁面温度达到拟临界温度或流体平均温度达到临界温度时产生的; 2. 换热系数随质量流量的增加或壁面热流的降低而增大; 3. 通过提高煤油的压力可以显著降低恶化现象.

关键词:航空煤油;传热恶化;超临界;数值研究

Darkslateblue:Affiliate; Royal Blue:Author; Turquoise:Article

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