Fluid Mechanics and Flight Mechanics

Effect of overheat degree on water spray atomization under flash boiling condition

  • MAO Yufeng ,
  • LI Yunze ,
  • WANG Jixiang
Expand
  • School of Aeronautic Science and Engineering, Beihang University, Beijing 100083, China

Received date: 2018-03-22

  Revised date: 2018-04-17

  Online published: 2018-04-17

Abstract

Heat load in spacecraft and aerospace shuttles, which generally work in space and upper atmosphere, is increasing, while the cooling ability of these vehicles is poor. This study researchs the atomization degree of water spray under the superheated condition, which can exert direct influence on the cooling ability of aerospace vehicles. A model for breakup of a single water droplet caused by bubble growth and aerodynamic force under the superheated condition is established, and a model for mass transfer and heat transfer is also proposed. The Lagrangian method is used to track and integrate all the droplets in the system. The effect of different degrees of superheat on spray atomization and droplet temperature is calculated using MATLAB. Then the degree of effect superheat degree on spray cooling is concluded. The calculation results indicate that the atomization degree under the flash boiling condition is much better than that under the sub-cooled condition. The droplet temperature will rapidly approach the boiling temperature under the superheated condition. The higher degree of superheat, the higher atomization degree, and thus the better spray cooling ability theoretically.

Cite this article

MAO Yufeng , LI Yunze , WANG Jixiang . Effect of overheat degree on water spray atomization under flash boiling condition[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018 , 39(S1) : 722184 -722184 . DOI: 10.7527/S1000-6893.2018.22184

References

[1] SHANMUGASUNDARAM V, RAMALINGAM M, DONOVAN B. Thermal management system with energy storage for an airborne laser power system application[C]//5th International Energy Conversion Engineering Conference and Exhibit (IECEC), 2007.
[2] 彭治雨, 石义雷, 龚红明, 等. 高超声速气动热预测技术及发展趋势[J]. 航空学报, 2015, 36(1):325-345. PENG Z Y, SHI Y L, GONG H M, et al. Hypersonic aeroheating prediction technique and its trend of development[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(1):325-345(in Chinese).
[3] 李翔, 傅波. 高超声速飞行器复杂结构热试验技术[J]. 航空学报, 2016, 37(S1):73-79. LI X, FU B. Thermal test technique of complex structure of hypersonic aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(S1):73-79(in Chinese).
[4] LEE S H, MUDAWAR I, HASAN MM. Thermal analysis of hybrid single-phase, two-phase and heat pump thermal control system (TCS) for future spacecraft[J]. Applied Thermal Engineering, 2016, 100:190-214.
[5] 侯增祺, 胡金刚. 航天器热控制技术[M]. 北京:中国科学技术出版社, 2007:129-293. HOU Z Q, HU J G. Thermal control technology for spacecraft[M]. Beijing:China Science and Technology Press, 2007:129-293(in Chinese).
[6] 汪新智, 马军军, 彭稳根, 等. 高超声速飞行器主动冷却系统优化设计[J]. 航空学报, 2014, 35(3):624-633. WANG X Z, MA J J, PENG W G, et al. Optimal design for active cooling system of hypersonic vehicle[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(3):624-633(in Chinese).
[7] WANG J X, LI Y Z, ZHANG H S, et al. Investigation of a spray cooling system with two nozzles for space application[J]. Applied Thermal Engineering, 2015, 89:115-124.
[8] SMAKULSKI P, PIETROWICZ S. A review of the capabilities of high heat flux removal by porous material, microchannels and spray cooling technologies[J]. Applied Thermal Engineering, 2016, 104:636-646.
[9] KIM J. Spray cooling heat transfer:The state of the art[J]. International Journal of Heat and Fluid Flow, 2007, 28(4):753-767.
[10] WANG J X, LI Y Z, YU X K, et al. Investigation of heat transfer mechanism of low environmental pressure large-space spray cooling for near-space flight systems[J]. International Journal of Heat and Mass Transfer, 2018, 119:496-507.
[11] 赵凯璇, 赵建福, 陈淑玲, 等. 液滴真空闪蒸/冻结过程的热动力学研究[J]. 中国空间科学学报, 2011, 31(1):57-62. ZHAO K X, ZHAO J F, CHEN S L, et al. Thermodynamic of flashing/freezing process of a droplet in vacuum[J]. Chinese Journal of Space Science, 2011, 31(1):57-62(in Chinese).
[12] WANG J X, LI Y Z, LI G C, et al. Investigation of a gravity-immune chip-level spray cooling for thermal protection of laser-based wireless power transmission system[J]. International Journal of Heat and Mass Transfer, 2017, 114:715-726.
[13] MUGELE R A, EVANS H D. Droplet size distribution in sprays[J]. Industrial & Engineering Chemistry, 1951, 43(6):1317-1324.
[14] SHER E, BAR-KOHANY T, RASHKOVAN A. Flash-boiling atomization[J]. Progress in Energy and Combustion Science, 2008, 34(4):417-439.
[15] ZENG Y, LEE C F F. An atomization model for flash-boiling sprays[J]. Combustion Science and Technology, 2001, 169(1):45-67.
[16] KAWANO D, ISHⅡ H, SUZUKI H,et al. Numerical study on flash-boiling spray of multicomponent fuel[J]. Heat Transfer-Asian Research, 2006, 35(5):369-385.
Outlines

/