Experimental Analysis on Characteristic and Boundary ofThermo-Acoustic Flow Instability in Hydrocarbon Fuel

doi:10.13675/j.cnki. tjjs. 180474

Journal of Propulsion Technology ›› 2019, Vol. 40 ›› Issue (8): 1817-1823.DOI: 10.13675/j.cnki. tjjs. 180474

Previous Articles Next Articles

Experimental Analysis on Characteristic and Boundary ofThermo-Acoustic Flow Instability in Hydrocarbon Fuel

1.School of Energy and Power Engineering,Northeast Electric Power University,Jilin 132012,China;2.School of Energy and Power Engineering,Dalian University of Technology,Dalian 116024,China

Published:2021-08-15

碳氢燃料热声不稳定流动特性和边界实验分析

1.东北电力大学能源与动力工程学院;2.大连理工大学能源与动力学院，辽宁大连;116024

基金资助:
国家自然科学基金 51576027;东北电力大学博士科研启动基金 BSJXM-2017205国家自然科学基金（51576027）；东北电力大学博士科研启动基金（BSJXM-2017205）。

Abstract

Abstract: In order to ensure the safe and stable operation of air-fuel heat exchanger, an experimental study on the thermo-acoustic flow instability of supercritical pressure aviation fuel in a vertical upward circular tube was conducted. The oscillation characteristic of wall temperature and the induced cause of thermo-acoustic flow instability were expounded. The effects of operating parameters on the border between flow stability conditions and flow instability conditions were described. Taking the averaged heat flux in the adjacent flow stability condition and flow instability condition as the boundary, variation of this boundary with the inlet pseudo-cooling degree was analyzed. The prediction criteria of thermo-acoustic flow instability boundary were established based on the ratio of critical pseudo-cooling number and pseudo-phase number which is related to the inlet Reynolds number and reduced pressure. Results show that the pseudo-boiling effect leads to the thermo-acoustic flow instability phenomenon. The lower the inlet fluid temperature and operating pressure, the more likely the thermo-acoustic flow instability will occur. The criteria for boundary prediction has a higher precision, the relative error with the experimental results is within ±15%.

Key words: Supercritical pressure;Aviation fuel;Thermo-acoustic instability;Characteristic;Boundary

摘要： 为保障空-油换热器安全稳定运行，对竖直上升圆管内超临界压力航空燃料的热声不稳定流动进行了实验研究。阐述了管壁温度的振荡特征和热声不稳定流动的诱发原因。考察了运行参数对流动稳定工况和流动不稳定工况界限的影响。取相邻流动稳定工况和流动不稳定工况的热流密度平均值作为边界，分析了该边界随进口拟过冷度的变化情况。通过临界拟相变数和拟过冷度数的比值表征，建立了热声不稳定流动边界与进口雷诺数和相对压力关联的预测准则。结果表明：拟沸腾效应导致了热声不稳定流动现象。进口温度和运行压力越低，热声不稳定流动越容易出现。提出的边界预测准则具有较高的精度，与实验结果的相对偏差在±15%以内。

关键词: 超临界压力;航空燃料;热声不稳定;特性;边界

References

[1] Deng H W, Zhu K， Xu G Q， et al. Heat Transfer Characteristics of RP-3 Kerosene at Supercritical Pressure in a Vertical Circular Tube[J]. Journal of Enhanced Heat Transfer， 2012， 19(5): 409-421.
[2] Zhang C B， Xu G Q， Gao L， et al. Experimental Investigation on Heat Transfer of a Speci?c Fuel(RP-3) Flows Through Downward Tubes at Supercritical Pressure[J]. Journal of Supercritical Fluids， 2012， 72(9): 90-99.
[3] Zhu K， Xu G Q， Tao Z， et al. Flow Frictional Resistance Characteristics of Kerosene RP-3 in Horizontal Circular Tube at Supercritical Pressure[J]. Experimental Thermal and Fluid Science， 2013， 44(1): 245-252.
[4] Huang D， Ruan B， Wu X Y， et al. Experimental Study on Heat Transfer of Aviation Kerosene in a Upward Tube at Supercritical Pressure[J]. Chinese Journal of Chemical Engineering， 2015， 23(2): 425-434.
[5] Zhong F Q， Fan X J， Yu G， et al. Heat Transfer of Aviation Kerosene at Supercritical Conditions[J]. Journal of Thermophysics and Heat Transfer， 2009， 23(3): 543-550.
[6] Liu Z H， Bi Q C， Guo Y， et al. Convective Heat Transfer and Pressure Drop Characteristics of Near-Critical-Pressure Hydrocarbon Fuel in a Minichannel[J]. Applied Thermal Engineering， 2013， 51(1-2): 1047-1054.
[7] Hines W S， Wolf H. Pressure Oscillations Associated with Heat Transfer to Hydrocarbon Fluids at Supercritical Pressures and Temperatures[J]. American Rocket Society Journal， 1962， 32(3): 361-366.
[8] Linne D L， Meyer M L， Edwards T， et al. Evaluation of Heat Transfer and Thermal Stability of Supercritical JP-7 Fuel[R]. AIAA97-3041.
[9] Brad H， Michael K. Experimental Investigation of Heat Transfer and Flow Instabilities in Supercritical Fuels[R]. AIAA97-3043.
[10] Brad H， Michael K. Enhancement of Heat Transfer and Elimination of Flow Oscillations in Supercritical Fuels[R]. AIAA98-3759.
[11] Wang H， Zhou J， Pan Y， et al. Experimental Investigation on the Characteristics of Thermo-Acoustic Instability in Hydrocarbon Fuel at Supercritical Pressures[J]. Acta Astronautica， 2016， 121: 29-38.
[12] Wang H， Zhou J， Pan Y， et al. Experimental Investigation on the Onset of Thermo-Acoustic Instability of Supercritical Hydrocarbon Fuel Flowing a Small-Scale Channel[J]. Acta Astronautica， 2015， 117: 296-304.
[13] Yan J J， Zhu Y H， Zhao R， et al. Experimental Investigation of the Flow and Heat Transfer Instabilities in n-Decane at Supercritical Pressures in a Vertical Tube[J]. International Journal of Heat and Mass Transfer， 2018， 120: 987-996.
[14] 严俊杰，赵然，闫帅，等. 超临界压力下竖直圆管内正癸烷对流换热不稳定性实验[J]. 推进技术， 2017， 38(2): 450-456.
[15] 王彦红，李素芬，东明，等. 超临界压力航空煤油热声振荡与传热恶化实验研究[J]. 推进技术， 2016， 37(3): 401-410.
[16] 王彦红，李素芬. 超临界压力下航空煤油热声振荡的特性和预测 [J]. 化工学报， 2018， 69(4): 1412-1418.
[17] Pan H， Bi Q C， Liu Z H， et al. Experimental Investigation on Thermo-Acoustic Instability and Heat Transfer of Supercritical Endothermic Hydrocarbon Fuel in a Mini Tube[J]. Experimental Thermal and Fluid Science， 2018， 97: 109-118.
[18] 胡江玉，周进，潘余，等. 超临界压力煤油传热不稳定实验研究[J]. 气体物理， 2017， 2(1): 57-63.
[19] Linne D L， Meyer M L， Braun D C. Investigation of Instabilities and Heat Transfer Phenomena in Supercritical Fuels at High Heat Flux and Temperatures[R]. AIAA2000- 3128.
[20] Zhou W X， Yu B， Qin J， et al. Mechanism and Influencing Factors Analysis of Flowing Instability of Supercritical Endothermic Hydrocarbon Fuel Within a Small-Scale Channel[J]. Applied Thermal Engineering， 2014， 71(1): 34-42.
[21] 张春本，邓宏武，徐国强，等. 超临界压力下航空煤油RP-3焓值的测量及换热研究[J]. 航空动力学报， 2010， 25(2): 331-335.
[22] Deng H W， Zhang C B， Xu G Q， et al. Density Measurements of Endothermic Hydrocarbon Fuel at Sub- and Supercritical Conditions[J]. Journal of Chemical and Engineering Data， 2011， 56(6): 2980-2986.
[23] Jia Z X， Xu G Q， Deng H W， et al. Experimental Measurements of Thermal Conductivity of Hydrocarbon Fuels by a Steady and Kinetic Method[J]. Journal of Thermal Analysis and Calorimetry， 2016， 123(1): 891-898.
[24] Deng H W， Zhang C B， Xu G Q， 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.
[25] 王彦红. 超临界压力航空煤油热声振荡与传热恶化的机理及预测研究[D]. 大连:大连理工大学， 2016.
[26] Jiang R P， Liu G Z， Zhang X W. Thermal Cracking of Hydrocarbon Aviation Fuels in Regenerative Cooling Microchannels[J]. Energy and Fuels， 2013， 27(5): 2563- 2577.
[27] Xu K K， Meng H. Modeling and Simulation of Supercritical Pressure Turbulent Heat Transfer of Aviation Kerosene with Detailed Pyrolytic Chemical Reactions[J]. Energy and Fuels， 2015， 29: 4137-4149.
[28] 李佳. 自然循环过冷沸腾流动不稳定性起始条件的研究[D]. 重庆:重庆大学， 2013.
[29] Ambrosini W， Sharabi M. Dimensionless Parameters in Stability Analysis of Heated Channels with Fluids at Supercritical Pressures[J]. Nuclear Engineering and Design， 2008， 238(8): 1917-1929.
[30] Yang Z Q， Shan Y F. Experimental Study on the Onset of Flow Instability in Small Horizontal Tubes at Supercritical Pressures[J]. Applied Thermal Engineering， 2018， 135(5): 504-511.

Experimental Analysis on Characteristic and Boundary ofThermo-Acoustic Flow Instability in Hydrocarbon Fuel

碳氢燃料热声不稳定流动特性和边界实验分析

PDF

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 0

Recommended Articles

Metrics

Comments