Effect of different species on physical properties for the surrogate of aviation fuel

PEI Xinyan; HOU Lingyun

doi:10.16511/j.cnki.qhdxxb.2017.25.036

PDF(1535 KB)

Journal of Tsinghua University(Science and Technology) ›› 2017, Vol. 57 ›› Issue (7) : 774-779. DOI: 10.16511/j.cnki.qhdxxb.2017.25.036

AEROSPACE AND ENGINEERING MECHANICS

Effect of different species on physical properties for the surrogate of aviation fuel

{{article.zuoZhe_EN}}

Author information +

History +

Abstract

Thermo-physical properties for surrogate aviation kerosene RP-3 were developed in this study to lay a foundation of the further investigation of the heat transfer calculation and experiment. The specific heat calculated from different surrogate models of the RP-3 was compared with the experimental data. The effects of three kinds of species, i.e. paraffin, cycloalkanes, benzenes, on thermo-physical properties were analyzed. There are the big differences of thermal properties at pseudo-critical temperatures. Based on the previous research of surrogate models and the GC-MS analysis of RP-3, a four-species surrogate was proposed. The numerical results for thermo-physical properties were in good agreement with the experimental data, including the specific heat, density and viscosity.

Key words

hydrocarbon fuel / RP-3 / surrogate model / supercritical condition

Cite this article

EndNote

Ris (Procite)

Bibtex

Download Citations

PEI Xinyan, HOU Lingyun. Effect of different species on physical properties for the surrogate of aviation fuel[J]. Journal of Tsinghua University(Science and Technology). 2017, 57(7): 774-779 https://doi.org/10.16511/j.cnki.qhdxxb.2017.25.036

References

[1] 朱锟, 邓宏武, 王英杰, 等. 超临界压力下航空煤油结焦换热综述及实验 [J]. 航空动力学报, 2010, 25(11):2472-2478.ZHU Kun, DENG Hongwu, WANG Yingjie, et al. Review and experimental study of the coke deposition and heat transfer characteristics of aviation kerosene at supercritical pressure [J]. Journal of Aerospace Power, 2010, 25(11):2472-2478. (in Chinese) [2] 范学军, 俞刚. 大庆RP-3航空煤油热物性分析 [J]. 推进技术, 2006, 27(2):187-192.FAN Xuejun, YU Gang. Analysis of thermophysical properties of Daqing RP-3 aviation kerosene [J]. Journal of Propulsion Technology, 2006, 27(2):187-192. (in Chinese) [3] FAN Xuejun, ZHONG Fengquan, YU Gong. Catalytic cracking of China No. 3 aviation kerosene under supercritical conditions [C]//44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Hartford, CT, USA:American Institute of Aeronautics and Astronautics, 2008. [4] 程迪, 王新竹, 范学军. RP-3煤油热物性替代模型研究 [C]//高超声速专题研讨会暨第五届全国高超声速科学技术会议. 桂林:中国力学学会, 2012.CHENG Di, WANG Xinzhu, FAN Xuejun. Thermophysical surrogate modeling of RP-3 aviation kerosene [C]//5th Hypersonic Technology Conferences. Guilin, China:Chinese Society of Theoretical and Applied Mechanics, 2012. (in Chinese) [5] ZHONG Fengquan, FAN Xuejun, YU Gong, et al. Heat transfer of aviation kerosene at supercritical conditions [C]//44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Hartford, CT, USA:American Institute of Aeronautics and Astronautics, 2008. [6] ZHANG Ruoling, JIANG Jin, LE Jia. The simulation of endothermic fuel flow in cooling channels of scramjet [C]//International Conference on Methods of Aerophysical Research, ICMAR. Akademgorodok, Novosibirsk, Russia:ICMAR, 2008. [7] 郑东, 于维铭, 钟北京. RP-3航空煤油替代燃料及其化学反应动力学模型 [J]. 物理化学学报, 2015, 31(4):636-642.ZHENG Dong, YU Weiming, ZHONG Beijing. RP-3 aviation kerosene surrogate fuel and the chemical reaction kinetic model [J]. Acta Phys Chim Sin, 2015, 31(4):636-642. (in Chinese) [8] JIANG Rongpei, LIU Guozhu, ZHANG Xiangwen. Thermal cracking of hydrocarbon aviation fuels in regenerative cooling microchannels [J]. Energy & Fuels, 2013, 27(5):2563-2577. [9] Huber M L, Smith B L, Ott L S, et al. Surrogate mixture model for the thermophysical properties of synthetic aviation fuel S-8:Explicit application of the advanced distillation curve [J]. Energy & Fuels, 2008, 22(2):1104-1114. [10] NIST Standard Reference Database 4. NIST Thermophysical Properties of Hydrocarbon Mixtures Database (SUPERTRAPP) [S]. Gaithersburg, MD, USA:National Inst. of Standards, 1999. [11] DENG Hongwu, ZHU Kun, XU Guoqiang, et al. Isobaric specific heat capacity measurement for kerosene RP-3 in the near-critical and supercritical regions [J]. Journal of Chemical & Engineering Data, 2012, 57(2):263-268. [12] Roan M A, Boehman A L. The effect of fuel composition and dissolved oxygen on deposit formation from potential JP-900 basestocks [J]. Energy & Fuels, 2004, 18(3):835-843. [13] DENG Hongwu, ZHANG Chunben, XU Guoqiang, et al. Density measurements of endothermic hydrocarbon fuel at sub- and supercritical conditions [J]. Journal of Chemical & Engineering Data, 2011, 56(6):2980-2986. [14] DENG Hongwu, ZHANG Chunben, XU Guoqiang, et al. Viscosity measurements of endothermic hydrocarbon fuel from 298 to 788 K under supercritical pressure conditions [J]. Journal of Chemical And Engineering Data, 2012, 57(2):358-365.