期刊文献+

Breakup of Cavitation Bubbles within the Diesel Droplet 被引量:4

Breakup of Cavitation Bubbles within the Diesel Droplet
下载PDF
导出
摘要 Supercavitation in the diesel nozzle increases the instability of droplets in part due to the two-phase mixture, while the effect of cavitation bubbles on the instability of drops is still unclear. In order to investigate the breakup of cavitation bubbles within the diesel droplet, a new mathematical model describing the disturbance growth rate of the diesel bubble instability is developed. The new mathematical model is applied to predict the effects of fluids viscosity on the stability of cavitation bubbles. The predicted values reveal that the comprehensive effect of fluids viscosity makes cavitation bubbles more stable. Compared with the viscosities of air and cavitation bubble, the diesel droplet's viscosity plays a dominant role on the stability of cavitation bubbles. Furthermore, based on the modified bubble breakup criterion, the effects of bubble growth speed, sound speed, droplet viscosity, droplet density, and bubble-droplet radius ratio on the breakup time and the breakup radius of cavitation bubbles are studied respectively. It is found that a bubble with large bubble-droplet radius ratio has the initial condition for breaking easily. For a given bubble-droplet radius ratio (0.2), as the bubble growth speed increases (from 2 m/s to 60 m/s), the bubble breakup time decreases(from 3.59 gs to 0.17 ps) rapidly. Both the greater diesel droplet viscosity and the greater diesel droplet density result in the increase of the breakup time. With increasing initial bubble-droplet radius ratio (from 0.2 to 0.8), the bubble breakup radius decreases (from 8.86 trn to 6.23 tm). There is a limited breakup radius for a bubble with a certain initial bubble-droplet radius ratio. The mathematical model and the modified bubble breakup criterion are helpful to improve the study on the breakup mechanism of the secondary diesel droplet under the condition of supercavitation. Supercavitation in the diesel nozzle increases the instability of droplets in part due to the two-phase mixture, while the effect of cavitation bubbles on the instability of drops is still unclear. In order to investigate the breakup of cavitation bubbles within the diesel droplet, a new mathematical model describing the disturbance growth rate of the diesel bubble instability is developed. The new mathematical model is applied to predict the effects of fluids viscosity on the stability of cavitation bubbles. The predicted values reveal that the comprehensive effect of fluids viscosity makes cavitation bubbles more stable. Compared with the viscosities of air and cavitation bubble, the diesel droplet's viscosity plays a dominant role on the stability of cavitation bubbles. Furthermore, based on the modified bubble breakup criterion, the effects of bubble growth speed, sound speed, droplet viscosity, droplet density, and bubble-droplet radius ratio on the breakup time and the breakup radius of cavitation bubbles are studied respectively. It is found that a bubble with large bubble-droplet radius ratio has the initial condition for breaking easily. For a given bubble-droplet radius ratio (0.2), as the bubble growth speed increases (from 2 m/s to 60 m/s), the bubble breakup time decreases(from 3.59 gs to 0.17 ps) rapidly. Both the greater diesel droplet viscosity and the greater diesel droplet density result in the increase of the breakup time. With increasing initial bubble-droplet radius ratio (from 0.2 to 0.8), the bubble breakup radius decreases (from 8.86 trn to 6.23 tm). There is a limited breakup radius for a bubble with a certain initial bubble-droplet radius ratio. The mathematical model and the modified bubble breakup criterion are helpful to improve the study on the breakup mechanism of the secondary diesel droplet under the condition of supercavitation.
出处 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2014年第1期198-204,共7页 中国机械工程学报(英文版)
基金 supported by National Natural Science Foundation of China(Grant No.51276011) Beijing Municipal Natural Science Foundation of China(Grant No.3132016) National Hi-tech Research and Development Program of China(863 Program,Grant No.2013AA065303) Opening Foundation of State Key Laboratory of Engines of China(Grant No.K2013-3)
关键词 SUPERCAVITATION INSTABILITY diesel droplet cavitation bubbles secondary breakup supercavitation, instability, diesel droplet, cavitation bubbles, secondary breakup
  • 相关文献

参考文献20

  • 1ZHAO Wei-guo,ZHANG Ling-xin,SHAO Xue-ming.NUMERICAL SIMULATION OF CAVITATION FLOW UNDER HIGH PRESSURE AND TEMPERATURE[J].Journal of Hydrodynamics,2011,23(3):289-294. 被引量:7
  • 2PAYRI R, GARCIAJ M, SALVADOR FJ, et al. Using spray momentum flux measurements to understand the influence of diesel nozzle geometry on spray characteristics[J]. Fuel, 2005, 84: 551-561.
  • 3SHI Suguo,WANG Guoyu.Numerical Calculation of Thermal Effect on Cavitation in Cryogenic Fluids[J].Chinese Journal of Mechanical Engineering,2012,25(6):1176-1183. 被引量:5
  • 4SARRE C V K, KONG S C, REITZ R D. Modeling the effects of injector nozzle geometry on diesel sprays[C]//SAE Paper, Melbourne, Australia,Jan 1, 1999: 1375-1388.
  • 5HE Z X, ZHONG WJ, WANG Q, et al. An investigation of transient nature of the cavitating flow in injector nozzles[J]. Applied Thermal Engineering, 2013, 54(1): 56-64.
  • 6SOU A, HOSOKA WA S, TOMIY A WA A. Effects of cavitation in a nozzle on liquidJet atomization[J]. InternationalJournal of Heat and Mass Transfer, 2007, 50fl7-18): 3 575-3 582.
  • 7GIORGI M G, FICARELLA A, TARANTINO M. Evaluating cavitation regimes in an internal orifice at different temperatures using frequency analysis and visualization[J]. InternationalJournal of Heat and Fluid Flow, 2013, 39: 160-172.
  • 8BLESSING M, KONIG G, KRUGER C, et al. Analysis of flow and cavitation phenomena in diesel injection nozzles and its effects on spray and mixture formation[C]IISAE Paper, Madison, Wisconsin, USA,Jan 1,2003-01-1358.
  • 9T AMAKI N. Effects of cavitation in a nozzle hole on atomization of spray and development of high-efficiency atomization enhancement nozzle[C]llllth Triennial International Annual Conference on Liquid Atomization and Spray Systems, Vail, Colorado, USA,July, 2009.
  • 10SAFARI S D. Effects of cavitation on high-pressure atomization[D]. California: University of California, Irvine, 2009.

二级参考文献42

  • 1CHEN Ying LU Chuan-jing WU Lei.MODELLING AND COMPUTATION OF UNSTEADY TURBULENT CAVITATION FLOWS[J].Journal of Hydrodynamics,2006,18(5):559-566. 被引量:21
  • 2UTTURKAR Y, WU J Y, WANG G Y, et al. Recent progress in modeling of cryogenic cavitation for liquid rocket propulsion[J]. Progress in Aerospace Sciences, 2005, 41: 558-608.
  • 3HORD J. Cavitation in liquid cryogens, II-Hydrofoil[R]. NASA Contractor Report, 1973a, NASA CR - 2156.
  • 4HORD J. Cavitation in liquid cryogens, llI-Ogives[R]. NASA Contractor Report, 1973b, NASA CR - 2242.
  • 5FRANC J P, REBATTET C, COUKON A. An experimental investigation of thermal effects in a cavitating inducer[J]. ASMEJournal of Fluids Engineering, 2004, 126(5): 716-723.
  • 6YOSHIDA Y, KIKUTA K, WATANABE M, et al. Thermodynamic effect on cavitation performances and cavitation instabilities in an inducer[C]//Proc, of 6th International Symposium on Cavitations, Wageningen, The Netherland, 2006, 38: 1-9.
  • 7STAHL H, STEPANOFF A. Thermodynamic aspects of cavitation in centrifugal pumps[J]. Journal of Basic Engineering, 1956, 78: 1 691-1 693.
  • 8RUGGERI R S, MOORE R D. Method of prediction of pump cavitation performance for various liquids, liquid temperatures and rotation speeds[R]. NASA Technical Note, 1969, NASA TN D-5292.
  • 9DESHPANDE M, FENG J Z, MERKLE C L. Numerical modelin of the thermodynamic effects of cavitation[J], d. Fluids Eng-Tram ASME, 1997, 119(2): 420-427.
  • 10TOKUMASU T, SEKINO Y, KAMIJO K. The numerical analysis of the effect of flow properties on the thermodynamic effect of cavitation[J]. Trans. Japan Soc. Aeron. Space Sci., 2004, 47(156): 146-152.

共引文献22

同被引文献36

引证文献4

二级引证文献2

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部