| Citation: | LIU Ruihang, SHAN Yong, ZHANG Jingzhou, et al. Experimental and numerical simulation researches on supercritical pressure aviation kerosene cooling[J]. Journal of Aerospace Power, 2026, 41（2）：20240401 doi: 10.13224/j.cnki.jasp.20240401
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To validate the cooling characteristics of supercritical pressure aviation kerosene on metal test sections under high thermal loads, numerical simulations were employed to obtain relevant experimental conditions. The influence of cooling water flow rate on the heat transfer within the test section walls was discussed. The experiments verified the impact of cooling fuel flow rate on the cooling effectiveness and the temperature distribution on the gas-side wall of the test section. Simulations were conducted to model the effect of gas inlet temperature distribution on the wall cooling performance. The following conclusions were drawn: for each cooling fuel flow rate, there existed a corresponding cooling water flow rate that minimized the impact of the water cooling channel on fuel cooling. As the cooling fuel flow rate increased, both the average and maximum temperatures on the gas side gradually decreased. Experimental data showed that under an average mainstream gas temperature of 904 K in the test section, when the cooling fuel flow rate reached its maximum value of 0.09 kg/s, the highest wall temperature on the gas side can be reduced to 539 K. The experimental values were slightly higher than the corresponding simulation values, with a simulation error within 12%, and the relationship between the maximum temperature of the gas side wall surface and the required cooling fuel flow per unit area of the gas-side wall surface was fitted into an empirical formula. Under the influence of
| [1] |
ZHU Yinhai, PENG Wei, XU Ruina, et al. Review on active thermal protection and its heat transfer for airbreathing hypersonic vehicles[J]. Chinese Journal of Aeronautics, 2018, 31(10): 1929-1953. doi: 10.1016/j.cja.2018.06.011
|
| [2] |
ZHANG Silong, LI Xin, ZUO Jingying, et al. Research progress on active thermal protection for hypersonic vehicles[J]. Progress in Aerospace Sciences, 2020, 119: 100646. doi: 10.1016/j.paerosci.2020.100646
|
| [3] |
章思龙, 秦江, 周伟星, 等. 高超声速推进再生冷却研究综述[J]. 推进技术, 2018, 39(10): 2177-2190. ZHANG Silong, QIN Jiang, ZHOU Weixing, et al. Review on regenerative cooling technology of hypersonic propulsion[J]. Journal of Propulsion Technology, 2018, 39(10): 2177-2190. (in Chinese
ZHANG Silong, QIN Jiang, ZHOU Weixing, et al. Review on regenerative cooling technology of hypersonic propulsion[J]. Journal of Propulsion Technology, 2018, 39(10): 2177-2190. (in Chinese)
|
| [4] |
鲍文, 章思龙, 秦江. 再生冷却超燃冲压发动机回热循环分析[R]. 无锡: 中国力学学会, 第三届高超声速科技学术会议, 2010.
|
| [5] |
姜蕾, 刘朝晖, 毕勤成, 等. 碳氢燃料变压力过程中传热研究[J]. 推进技术, 2014, 35(7): 965-972. JIANG Lei, LIU Zhaohui, BI Qincheng, et al. Heat transfer of hydrocarbon fuel during transient pressure[J]. Journal of Propulsion Technology, 2014, 35(7): 965-972. (in Chinese
JIANG Lei, LIU Zhaohui, BI Qincheng, et al. Heat transfer of hydrocarbon fuel during transient pressure[J]. Journal of Propulsion Technology, 2014, 35(7): 965-972. (in Chinese)
|
| [6] |
王夕, 刘波, 祝银海, 等. 超临界压力下RP-3在细圆管内对流换热实验研究[J]. 工程热物理学报, 2015, 36(2): 360-365. WANG Xi, LIU Bo, ZHU Yinhai, et al. Experimental investigation on convection heat transfer of supercritical pressure RP-3 in a small pipe[J]. Journal of Engineering Thermophysics, 2015, 36(2): 360-365. (in Chinese
WANG Xi, LIU Bo, ZHU Yinhai, et al. Experimental investigation on convection heat transfer of supercritical pressure RP-3 in a small pipe[J]. Journal of Engineering Thermophysics, 2015, 36(2): 360-365. (in Chinese)
|
| [7] |
胡江玉, 周进, 潘余, 等. 竖直圆管内超临界压力煤油传热特性实验研究[J]. 气体物理, 2016, 1(4): 51-57. HU Jiangyu, ZHOU Jin, PAN Yu, et al. Experimental investigation on heat transfer of kerosene flowing in a vertical tube at supercritical pressure[J]. Physics of Gases, 2016, 1(4): 51-57. (in Chinese
HU Jiangyu, ZHOU Jin, PAN Yu, et al. Experimental investigation on heat transfer of kerosene flowing in a vertical tube at supercritical pressure[J]. Physics of Gases, 2016, 1(4): 51-57. (in Chinese)
|
| [8] |
史一诺, 单勇, 谭晓茗, 等. 冲压发动机喷管超临界压力燃油冷却特性[J]. 航空动力学报, 2024, 39(10): 20220704. SHI Yinuo, SHAN Yong, TAN Xiaoming, et al. Cooling characteristics of supercritical pressure fuel in ramjet nozzle[J]. Journal of Aerospace Power, 2024, 39(10): 20220704. (in Chinese
SHI Yinuo, SHAN Yong, TAN Xiaoming, et al. Cooling characteristics of supercritical pressure fuel in ramjet nozzle[J]. Journal of Aerospace Power, 2024, 39(10): 20220704. (in Chinese)
|
| [9] |
张卓远, 黄世璋, 高效伟. 超临界压力下正癸烷在水平矩形冷却通道内的流动传热数值模拟[J]. 航空学报, 2018, 39(12): 122297. ZHANG Zhuoyuan, HUANG Shizhang, GAO Xiaowei. Numerical simulation of heat transfer of n-decane under supercritical pressure in horizontal rectangular cooling channels[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(12): 122297. (in Chinese
ZHANG Zhuoyuan, HUANG Shizhang, GAO Xiaowei. Numerical simulation of heat transfer of n-decane under supercritical pressure in horizontal rectangular cooling channels[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(12): 122297. (in Chinese)
|
| [10] |
刘朝晖, 宋晨阳, 陈强, 等. 超(近)临界压力航空煤油RP-3的拟过冷沸腾传热特性[J]. 推进技术, 2021, 42(6): 1418-1424. LIU Zhaohui, SONG Chenyang, CHEN Qiang, et al. Pseudo subcooled boiling heat transfer characteristics of aviation kerosene RP-3 under super-and near-critical pressure conditions[J]. Journal of Propulsion Technology, 2021, 42(6): 1418-1424. (in Chinese
LIU Zhaohui, SONG Chenyang, CHEN Qiang, et al. Pseudo subcooled boiling heat transfer characteristics of aviation kerosene RP-3 under super-and near-critical pressure conditions[J]. Journal of Propulsion Technology, 2021, 42(6): 1418-1424. (in Chinese)
|
| [11] |
郭世哲. 矩形通道内超临界碳氢燃料流动及强化换热研究[D]. 南京: 南京航空航天大学, 2022. GUO Shizhe. Research on flow and enhanced heat transfer of supercritical hydrocarbon fuel in rectangular channel[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2022. (in Chinese
GUO Shizhe. Research on flow and enhanced heat transfer of supercritical hydrocarbon fuel in rectangular channel[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2022. (in Chinese)
|
| [12] |
谢凯利. 小尺度矩形通道内碳氢燃料流动及强化传热研究[D]. 哈尔滨: 哈尔滨工业大学, 2015. XIE Kaili. Study on flow and enhanced heat transfer of hydrocarbon fuel in samall-scale rectangular channels[D]. Harbin: Harbin Institute of Technology, 2015. (in Chinese
XIE Kaili. Study on flow and enhanced heat transfer of hydrocarbon fuel in samall-scale rectangular channels[D]. Harbin: Harbin Institute of Technology, 2015. (in Chinese)
|
| [13] |
孙士平, 徐德辉, 刘道煌, 等. 主动冷却薄壁结构的通道布局与形状优化[J]. 航空动力学报, 2022, 37(1): 1-10. SUN Shiping, XU Dehui, LIU Daohuang, et al. Channel layout and shape optimization of active cooling thin-walled structures[J]. Journal of Aerospace Power, 2022, 37(1): 1-10. (in Chinese
SUN Shiping, XU Dehui, LIU Daohuang, et al. Channel layout and shape optimization of active cooling thin-walled structures[J]. Journal of Aerospace Power, 2022, 37(1): 1-10. (in Chinese)
|
| [14] |
蒋劲, 张若凌, 乐嘉陵, 等. 燃油冷却面板传热特性试验与计算分析研究[J]. 实验流体力学, 2011, 25(1): 1-6. JIANG Jin, ZHANG Ruoling, LE Jialing, et al. The investigation on heat transfer characteristic tests and thermal evaluation of fuel-cooled panels[J]. Journal of Experiments in Fluid Mechanics, 2011, 25(1): 1-6. (in Chinese
JIANG Jin, ZHANG Ruoling, LE Jialing, et al. The investigation on heat transfer characteristic tests and thermal evaluation of fuel-cooled panels[J]. Journal of Experiments in Fluid Mechanics, 2011, 25(1): 1-6. (in Chinese)
|
| [15] |
LU Yang, WANG Xinzhu, LI Long, et al. Development and preliminary validation of a thermal analysis method for hydrocarbon regenerative-cooled supersonic combustor[R]. AIAA-2015-3556, 2015.
|
| [16] |
MUKHERJEE R, GOPINATH N K, VIGNESH V, et al. Thermal analysis of scramjet combustor panel with active cooling using cellular materials[C]//30th International Symposium on Shock Waves 1. Cham, US: Springer International Publishing, 2017: 239-244.
|
| [17] |
WIETING A R, GUY R W. Thermal-structural design/analysis of an airframe-integrated hydrogen-cooled scramjet[J]. Journal of Aircraft, 1976, 13(3): 192-197. doi: 10.2514/3.58649
|
| [18] |
The evolution of the hyset hydrocarbon fueled scramjet engine[R]. AIAA-2003-7005, 2003.
|
| [19] |
牛文, 李文杰. 美国空军圆满完成X-51A第四次试飞[J]. 飞航导弹, 2013(5): 3-4, 1. NIU Wen, LI Wenjie. The US Air Force successfully completed the fourth test flight of the X-51A[J]. Aerodynamic Missile Journal, 2013(5): 3-4, 1. (in Chinese
NIU Wen, LI Wenjie. The US Air Force successfully completed the fourth test flight of the X-51A[J]. Aerodynamic Missile Journal, 2013(5): 3-4, 1. (in Chinese)
|
| [20] |
TAO Zhi, CHENG Zeyuan, ZHU Jianqin, et al. Effect of turbulence models on predicting convective heat transfer to hydrocarbon fuel at supercritical pressure[J]. Chinese Journal of Aeronautics, 2016, 29(5): 1247-1261. doi: 10.1016/j.cja.2016.08.007
|
| [21] |
MENTER F R. Two-equation eddy-viscosity turbulence models for engineering applications[J]. AIAA Journal, 1994, 32(8): 1598-1605. doi: 10.2514/3.12149
|
| [22] |
HUBER M L. REFPROP, NIST thermodynamic properties of refrigerant mixtures database, Vision4.0: Version9.0 User's Guide [R]. Gaithersburg, US: National Institute of Standards and Technology(NIST), 2007.
|
| [23] |
陶文铨. 传热学[M]. 5版. 北京: 高等教育出版社, 2019.
|
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