期刊文献+

低频压力振荡环境下运动液滴蒸发过程的准稳态模型 被引量:5

Quasi-steady model of moving droplet evaporation process under low frequency pressure oscillation
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摘要 为了获得运动液滴蒸发过程对压力震荡的响应特性,从宏观上对压力振荡环境下的液滴蒸发过程进行了分析,压力振荡会引起液滴周围边界层内蒸汽质量分数的振荡,从而引起液滴蒸发速率的振荡。根据折算薄膜理论,提出了折算饱和蒸汽边界层的概念,基于已有的液滴蒸发准稳态模型,建立了压力振荡环境下运动液滴蒸发过程的准稳态模型,并进行数值求解,结果表明,液滴蒸发过程对低频压力震荡具有很强的响应能力,尤其对压力震荡幅值、频率比较敏感。 In order to obtain the response characteristics of moving droplet evaporation process under low frequency pressure oscillation,the process of droplet evaporation under pressure oscillation is analyzed in a level of macroscopic view.It indicates that pressure oscillation can bring the oscillation of vapor mass fraction in the boundary layer around droplet,and induces the droplet evaporation rate oscillation.According to the converted film theory,a concept of the converted saturation vapor boundary layer is presented.The quasi-steady model of moving droplet evaporation process with pressure oscillation is constructed based on the existent quasi-steady model of droplet evaporation,and resolved numerically.The results show that moving droplet evaporation process has strong response ability to pressure oscillation,especially sensitive to pressure oscillation amplitude and frequency.
出处 《推进技术》 EI CAS CSCD 北大核心 2011年第5期670-675,共6页 Journal of Propulsion Technology
基金 国家自然科学基金(51076168)
关键词 压力振荡 运动液滴 蒸发 准稳态 Pressure oscillation Moving droplet Evaporation Quasi-steady
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参考文献8

  • 1Priem R J, Guentert D C. Combustion instability limits determined by a nonlinear theory and a one-dimensional model[R]. NASA, TN D-1409 , 1962.
  • 2Lee G Y, Kim S Y , Yoon W S. Oscillatory vaporization and acoustic response of droplet at high pressure[ J]. Internal Communications in Heat and Mass Transfer, 2008, (35) :1302-1306.
  • 3Sheu W J, Liou N C. Effect of temporal variation of pressure on vaporization of liquid droplets[ J ]. Internal Journal of Heat and Mass Transfer, 1999, (42) :4043-4054.
  • 4Kim S Y, Yoon W S. Responses of droplet evaporation to high-pressure oscillations [ R ]. AIAA 2004-1161.
  • 5Saito M, Hoshikawa M,Sato M. Enhancement of evaporation/combustion rate coefficient of a single fuel droplet by acoustic oscillation [ J ]. Fuel, 1996, 75 ( 6 ) : 669-674.
  • 6Sujith R I, Waldherr G A, Jagoda J I, et al. Experimental investigation of the evaporation of droplets in axial acoustic fields[ R]. AIAA 1995-0495.
  • 7刘卫东,周进,王振国.振荡环境下推进剂液滴亚临界蒸发响应特性[J].航空动力学报,2001,16(1):52-54. 被引量:9
  • 8苏凌宇,于江飞,刘卫东.乙醇液滴蒸发过程对压力振荡动态响应的试验研究[J].推进技术,2009,30(3):286-291. 被引量:5

二级参考文献8

  • 1庄逢辰.液体火箭发动机喷雾燃烧的理论、模型及应用[M].国防科技大学出版社,1995..
  • 2Yang V,Progress in Astronautics and Aeronauticas Series,1996年,169页
  • 3庄逢辰,液体火箭发动机喷雾燃烧的理论、模型及应用,1995年
  • 4Yang V,AIAA 912310
  • 5(美)V.杨,(美)W.E.安德松主编,张宝炯等.液体火箭发动机燃烧不稳定性[M]科学出版社,2001.
  • 6[美]哈杰(D·T·Harrje)等 著,朱宁昌,张宝炯.液体推进剂火箭发动机不稳定燃烧[M]国防工业出版社,1980.
  • 7马友光,汪晓红,成弘,余国琮.气泡传质过程近界面非稳态特性及热力学研究[J].化学工程,2000,28(3):6-9. 被引量:6
  • 8刘朝,张新铭,谭宁,曾丹苓.汽液界面厚度和分维数[J].工程热物理学报,2004,25(4):562-564. 被引量:3

共引文献11

同被引文献42

  • 1田章福,陶玉静,苏凌宇,周进.多组分液滴蒸发过程的理论模型及试验研究[J].推进技术,2006,27(6):568-571. 被引量:11
  • 2杨V 安德松WE.张宝炯 洪鑫 陈杰 译.液体火箭发动机燃烧不稳定性[M].北京:科学出版社,2001..
  • 3何立明,严传俊,范玮,汪林全.混合气体燃烧中爆震波传播机理的研究[J].推进技术,1997,18(2):39-43. 被引量:10
  • 4聂万胜,丰松江.液体火箭发动机燃烧动力学模型与数值计算[M].北京:国防工业出版社.2011.
  • 5S.S. Sazhin,A. Elwardany,P.A. Krutitskii,G. Castanet,F. Lemoine,E.M. Sazhina,M.R. Heikal.A simplified model for bi-component droplet heating and evaporation[J].International Journal of Heat and Mass Transfer.2010(21)
  • 6C. Maqua,G. Castanet,F. Lemoine.Bicomponent droplets evaporation: Temperature measurements and modelling[J].Fuel.2008(13)
  • 7William L.H. Hallett.A simple model for the vaporization of droplets with large numbers of components[J].Combustion and Flame.2000(1)
  • 8Pecochin V R. Excitation of acoustic vibrations upon combustion of droplets of liquid fuel at supercritical pres- sure [J]. High Temperature, 2011, 49(6)- 906-910.
  • 9Dattarajan S, Lutomirski A, Lobbia R, et al. Acoustic excitation of droplet combustion in microgravity and normal gravity EJ]. Combustion and Flame, 2006, 144(1/2) ~ 299-317.
  • 10Tanabe M, Morita T, Aoki K, et al. Influence of standing sound waves on droplet combustion EJ]. Pro- ceedings of the Combustion Institute, 2000, 28(1): 1007-1013.

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