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研究生: 唐紹文
Tang, Marx
論文名稱: 同軸噴流破碎機制之實驗研究
An Experimental Study of the Breakup Mechanism of Coaxial Jet Spray
指導教授: 袁曉峰
Yuan, Tony
學位類別: 博士
Doctor
系所名稱: 工學院 - 航空太空工程學系
Department of Aeronautics & Astronautics
論文出版年: 2015
畢業學年度: 103
語文別: 英文
論文頁數: 98
中文關鍵詞: 同軸噴注器氣層厚度表面張力黏滯係數螺旋式運動帶狀液膜
外文關鍵詞: coaxial injector, gas layer thickness, surface tension, viscosity, spiral-type turning, ligament
相關次數: 點閱:98下載:32
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  • 同軸式噴注器多用於大推力之液態火箭引擎,主要功能為霧化燃燒所需之液態氧化劑與氣態燃料。本研究採用光學技術探討影響同軸噴流破碎及霧化混合之相關參數,如速度比(gas to liquid velocity ratio, varied from 2.9 to 60)、氣層厚度(gas layer thickness, varied from 1.2 mm to 2.4 mm)及液體的物理性質(表面張力及黏滯係數)。在實驗分析方面,本研究採用霧化角、平均粒徑、核心粒徑等指標並配合高速攝影觀察噴流之破碎機制、過程等,藉此分析相關參數對同軸噴流於不同實驗條件設定狀態下之影響。
    實驗結果顯示,外圍高速氣流是影響此同軸流場的重要因素,氣層除限制同軸噴流的空間分布外,主要為增強液柱本身的不穩定性使其進入螺旋式運動(spiral-type motion),液柱於此運動中拉伸並形成帶狀液膜(ligament)而破碎。對於中低速度比之噴流來說(即VR<15),當液注破碎後進入次霧化區時(secondary breakup region),此時外圍氣流與液滴的速度差已不足以使液滴再次破碎,氣體對霧化後的流場本身無顯著的影響。在這樣的機制控制下之同軸噴流,其霧化角會隨著氣液間速度比的提升而增加,並隨氣層厚度增加而下降。破碎霧化後的同軸噴流之平均粒徑呈現均勻、中心較集中且穩定的分布。
    於使用低表面張力液體之同軸噴流中可觀察到大量呈纖維狀分支之液膜。高速氣流之剪力作用於纖維狀液膜,可使更多細小的粒滴破碎並脫離液柱表面,此機制使噴流的平均粒徑下降。增加工作流體的黏滯係數對於同軸噴流有強烈之影響,高黏滯係數液體本身之聚合力可在螺旋運動狀態下之帶狀液膜破碎前,使其向外伸展而穿透氣液交界,液柱可藉由此機制增加高速氣流與液柱表面間之作用面積,進而更有效的利用高速氣流協助其霧化。故在高黏滯係數液體的同軸噴流中可觀察到較大的霧化角及較小的平均粒徑及核心粒徑。

    Coaxial injector is mainly used in large-scale liquid rocket engines. By utilizing optical methods, this research studies the effects of gas to liquid velocity ratio (2.9 to 60), gas layer thickness (1.2 mm to 2.4 mm), and liquid physical properties (surface tension and viscosity) on the breakup and atomization of coaxial liquid jet spray. The spray angles, droplet size (SMD, SMD0.1) distributions as well as the breakup processes at different experimental conditions are observed and analyzed.
    The results reveal that the significance of the breakup of coaxial jet spray is the surrounding high speed air confines the spray spatially, and forces the inherent unstable liquid column into spiral-type turning, then elongates into ligament before instantaneous breakup. Once the liquid jet has broken up, the outer high speed air appears to have no further effect on the spray. Due to this controlling breakup process, the spray angle appears to be increased with increasing velocity ratio but decreased with increasing gas layer thickness, and the droplet size distribution of coaxial jet spray appears to be uniform, concentrated, and invariant after jet has broken up.
    Coaxial jet with a lower liquid surface tension apparently shows more branching fiber growth from the liquid column surface that induces smaller droplets stripping from main wavy jet. Increasing liquid viscosity in this study shows an intense effect on coaxial jet spray. With higher viscosity, the liquid ligament is stretched wider to penetrate the liquid and gas boundary before disintegration. Hence, the liquid ligament could utilize more energy of surrounding high speed air for liquid atomization, thus to produce larger spray angle and smaller droplet sizes as observed in the experiments.

    CONTENTS ABSTRACT IN CHINESE I ABSTRACT XVIII ACKNOWLEDGEMENT XX CONTENTS XXI LIST OF TABLES XXII LIST OF FIGURES XXIII NOMENCLATURE XXVII CHAPTER I INTRODUCTION 1 1.1 LITERATURE REVIEW 2 1.2 MOTIVATION AND OBJECTIVE 10 CHAPTER II EXPERIMENTAL APPARATUS AND TECHNIQUES 12 2.1 EXPERIMENTAL DESIGN 12 2.2 APPARATUS 14 2.3 OPTICAL TECHNIQUES 18 CHAPTER III EXPERIMENTAL RESULTS AND ANALYSES 27 3.1 GAS LAYER THICKNESS 27 3.2 VELOCITY RATIO 28 3.2.1 Effects of Velocity Ratio on Spray Angle 28 3.2.2 Effects of Velocity Ratio on Droplet Size 31 3.3 LIQUID PHYSICAL PROPERTIES 34 3.3.1 Effects of Liquid Surface Tension 34 3.3.2 Effects of Liquid Viscosity 36 CHAPTER IV CONCLUSION AND FUTURE WORK 40 REFERENCES 45 APPENDIX A VELOCITY DISTRIBUTION OF SURROUNDING GAS STREAM 48 APPENDIX B SPRAY ANGLES OF COAXIAL JET SPRAYS AT DIFFERENT NON-DIMENSIONAL PARAMETERS 54 PUBLICATION LIST 96 VITA 98

    Chandrasekhar, S., Hydrodynamic and Hydromagnetic Stability, Dover, USA, 1961.
    Chigier, N. and Farago, Z., “Morphological Classification of Disintegration of Round Liquid Jets in a Coaxial Air Stream,” Atomization and Sprays, Vol. 2, No. 2, pp. 137-153, 1992.
    Chigier, N. and Reitz, R.D., “Regimes of Jet Breakup and Breakup Mechanisms (Physical Aspects),” Recent Advances in Spray Combustion: Spray Atomization and Drop Burning Phenomena, edited by K.K. Kuo, American Institute of Aeronautics and Astronautics, Virginia, pp. 109-135, 1996.
    Dombrowski, N. and Johns, W.R., “The Aerodynamic Instability and Disintegration of Viscous Liquid Sheets,” Chem. Eng Sci., Vol. 18, No. 3, pp. 203-214, 1963.
    Eckbreth, A.C., “Laser Diagnostics for Combustion Temperature and Species,” Gordon and Breach Science Publishers, the Netherlands, 1996.
    Engelbert, C., Hardalupas, Y., and White Law, J.H., “Breakup Phenomena in Coaxial Airblast Atomizers,” Proc. Mathematical and Physical Sciences, Vol. 451, No. 1941, pp. 189-229, 1995.
    Eroglu, H., Chigier, N. and Farago, Z., “Coaxial Atomizer Liquid Intact Lengths,” Phy. Fluids A, Vol. 3, pp. 303-308, 1991.
    Gautam, V. and Gupta, A.K., “Cryogenic Flow and Atomization from a Coaxial Injector,” Journal of Propulsion and Power, Vol. 25, No. 1, pp. 33-39, 2009.
    Hardalupas, Y. and Whitelaw, J.H., “Characteristics of Sprays Produced by Coaxial Airblast Atomizers,” Journal of Propulsion and Power, Vol. 10, No. 4, pp. 453-460, 1994.
    Hinze, J.O., “Fundamentals of the Hydrodynamic Mechanism of Splitting in Dispersion Processes,” AIChE J., Vol. 1, No. 3, pp.289-295, 1955.
    Hirt, C.W. and Nichols, B.D., “Volume-of Fluid (VOF) Method for the Dynamics of Free Boundaries,“ Journal of Computational Physics, Vol. 39, pp. 201-225, 1981.
    Hoyt, J.W. and Taylor, J.J., “Waves on Water Jets,” J. Fluid Mech., Vol. 83, No. 1, pp 119-127, 1977.
    Lasheras, J.C., Villermaux, E., and Hopfinger, E.J., “Break-up and Atomization of a Round Water Jet by a High-Speed Annular Air Jet,” J. Fluid Mech., Vol. 357, pp. 351-379, 1998.
    Lasheras, J.C. and Hopfinger, E.J., “Liquid Jet Instability and Atomization in a Coaxial Gas Stream,” Annu. Rev. Fluid Mech., Vol. 32, pp. 275–308, 2000.
    Lawn, C.J., “The Determination of the Rate of Dissipation in Turbulent Pipe Flow,” J. Fluid Mech., Vol. 48, Pt. 3, pp. 477-505, 1971.
    Lefebvre, A.H., Atomization and Sprays, Hemisphere Publishing, Washington, D.C., 1989.
    Lin, S.P. and Reitz, R.D., “Drop and Spray Formation from a Liquid Jet,” Annu. Rev. Fluid Mech., Vol. 30, No. 1, pp. 85-105, 1998.
    Lorenzetto, G.E. and Lefebvre, A.H., “Measurements of Drop Size on a Plain-Jet Airblast Atomizer,” AIAA J., Vol. 15, No. 7, pp. 1006-1010, 1977.
    Lux, J. and Haidn, O., “Effect of Recess in High-Pressure Liquid Oxygen/Methane Coaxial Injection and Combustion,” Journal of Propulsion and Power, Vol. 25, No. 1, pp. 24-32, 2009
    Mayer, W.O.H., “Coaxial Atomization of a Round Liquid Jet in a High Speed Gas Stream: A Phenomenological Study,” Experiments in Fluids, Vol. 16, No. 6, pp. 401-410, 1994.
    Mayer, W.O.H. and Krulle, G., “Rocket Engine Coaxial Injector Liquid/Gas Interface Flow Phenomena,” Journal of Propulsion and Power, Vol. 11, No. 3, pp. 513-519, 1995.
    Mayer, W.O.H. and Branam, R., “Atomization Characteristics on the Surface of a Round Liquid Jet,” Experiments in Fluids, Vol. 36, No. 4, pp. 528-539, 2004.
    Ohnesorge, W., “Formation of Drops by Nozzles and Breakup of Liquid Jets,” Z. Angew. Math. Mech., Vol. 16, pp. 355-358, 1936.
    Pan, Y. and Suga, K., “A Numerical Study on the Breakup Process of Laminar Liquid Jets into a Gas,” Phys. Fluids, Vol. 18, No. 5, p052101, 2006.
    Rayleigh, L., “On the Instability of Jets,” Proceedings of the London Math. Soc., Vol. 10, pp. 4-13, 1879.
    Rehab, H., Villermaux, E., and Hopfinger, E.J., “Flow Regimes of Large-Velocity-Ratio Coaxial Jets,” J. Fluid Mech., Vol. 345, pp. 357-381, 1997.
    Reitz, R.D., “Atomization and Other Breakup Regimes of a Liquid Jet,” Ph. D. Dissertation, Princeton University, Princeton, NJ, 1978.
    Reitz, R.D. and Bracco, F.V., “Mechanisms of Atomization of a Liquid Jet,” Phys. Fluids, Vol. 25, No. 10, pp. 1730-1742, 1982.
    Rizk, N.K. and Lefebvre, A.H., “Spray Characteristics of Plain-Jet Airblast Atomizers,” J. Eng. Gas Turbines Power, Vol. 106, No. 3, pp. 634-638, 1984.
    Ruff, G.A., Sagar, A.D., and Faeth, G.M., “Structure and Mixing Properties of Pressure-Atomized Sprays,” AIAA J., Vol. 27, pp. 549-559, 1989.
    Talley, D.G., Verdieck, J.F., Lee, S.W., McDonell, V.G., and Samuelsen, G.S., “Accounting for Laser Sheet Extinction in Applying PLIF to Sprays,” 34th Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA Paper No. AIAA-96-0469, 1996.
    Tseng, L.-K., Ruff, G.A., and Faeth, G.M., “Effects of Gas Density on the Structure of Liquid Jets in Still Gases,” AIAA J., Vol. 30, No. 6, pp. 1537-1544, 1992.
    Weber, C., “Zum zerfall eines flussigkeitstrahles (Disruption of Liquid Jets),” Z. Angew. Math. Mech., Vol. 2, No. 2, pp. 136-159, 1931.
    Wu, P.-K., Tseng, L.-K., and Faeth, G.M., “Primary Breakup in Gas/Liquid Mixing Layers for Turbulent Liquid,” Atomization and Sprays, Vol. 2, pp. 295-317, 1992.
    Yang, B., Cuoco, F., and Oschward, M., “Atomization and Flames in LOX/H2- and LOX/CH4- Spray combustion,” Journal of Propulsion and Power, Vol. 23, No. 4, pp. 763-771, 2007.
    Yuan, T., Chen, C., and Huang, B., “Optical Observation of the Impingements of Nitrogen Tetroxide/Monomethylhydrazine Simulants,” AIAA J., Vol. 44, No. 10, pp. 2259-2266, 2006.
    Yuan, T. and Huang, B., “Optical Analysis of the Mixing Effect in Fully Developed Like-Doublet Impinging Jet Sprays,” Atomization and Sprays, Vol. 22, No. 5, pp. 391-408, 2012.

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