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Liquid Jet Blasting Using Ultra-High Frequency Supersonic Pulsed Air Jet

DOI: 10.4236/jfcmv.2022.102004, PP. 57-75

Keywords: Ultrasonic Actuators, Flow Control, Liquid Blasting

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Abstract:

This paper reports an experimental study on a liquid injector assembly integrated with an ultra-high frequency pulsed air jet that operates at 21 kHz. The active air-blasting assembly steadily injects a liquid through four micro-nozzles of 0.4 mm diameters each, positioned around a 1 mm nozzle through which the pulsed actuation jet flows out at supersonic velocity. High-frequency compressible air vortexes and shock waves generated by the injector atomize the liquid stream into finer droplets and distribute them to a larger area to improve mixing with the ambiance. The paper presents the design details and preliminary studies on the flow field characteristics of this novel injection scheme, which is a potential candidate for high-speed flow mixing and control applications.

References

[1]  Burick, R.J. (1972) Space Storable Propellant Performance Program Coaxial Injectors Characterization. NASA-CR-120936.
[2]  Lefevvre, A.H. (1989) Atomization and Sprays. Tailor and Francis CRC Press, Boca Raton.
https://doi.org/10.1201/9781482227857
[3]  Gomi, H. (1985) Pneumatic Atomization with Coaxial Injectors: Measurements of Drop Sizes by the Diffraction Method and Liquid Phase Fraction by the Attenuation Method of Light. NAL-TR-888T, N 86-27595.
[4]  Hoyt, J.W. and Tailor, J.J. (1977) Waves on Water Jets. Journal of Fluid Mechanics, 83, 119-127.
https://doi.org/10.1017/S0022112077001074
[5]  Lasheras, J.C., Villermaux, E.V. and Hopfinger, E.J. (1998) Breakup and Atomization of a Round Water Jet by a High-Speed Annular Air Jet. Journal of Fluid Mechanics, 357, 351-379.
https://doi.org/10.1017/S0022112097008070
[6]  Eroglu, H., Chigier, N. and Farago, Z. (1991) Coaxial Atomizer Liquid Intact Lengths. Physics of Fluids, 3, 303-308.
https://doi.org/10.1063/1.858139
[7]  Engelbert, C., Hardalupas, Y. and Whitelaw, J.H. (1995) Breakup Phenomena in Coaxial Airblast Atomizers. Proceedings of the Royal Society of London, Series A, Mathematical, Physical and Engineering Sciences, 451, 189-229.
https://doi.org/10.1098/rspa.1995.0123
[8]  Lin, S. and Reitz, R. (1998) Drop and Spray Formation from a Liquid Jet. Annual Review of Fluid Mechanics, 30, 85-105.
https://doi.org/10.1146/annurev.fluid.30.1.85
[9]  Abhijeet, K. and Srikrishna, S. (2018) Liquid Jet Breakup Unsteadiness in a Coaxial Airblast Atomizer. International Journal of Spray and Combustion Dynamics, 10, 211-230.
https://doi.org/10.1177/1756827718760905
[10]  Reitz, R. and Bracco, F. (1982) Mechanism of Atomization of a Liquid Jet. The Physics of Fluids, 25, 1730-1742.
https://doi.org/10.1063/1.863650
[11]  Zhao, H., Liu, H.F., Tian, X.S., Xu, J.L., Li, W.F. amd Lin, K.F. (2014) Influence of Atomizer Exit Area Ratio on the Breakup Morphology of Coaxial Air And Round Water Jets. AIChE Journal, 60, 2335-2345.
https://doi.org/10.1002/aic.14414
[12]  Kolmogorov, A.N. (1949) On the Disintegration of Drops by Turbulent Flows. Doklady Akademii Nauk SSSR, 66, 825-828.
[13]  Hinze, J.O. (1955) Fundamentals of the Hydrodynamic Mechanism of Splitting in Dispersion Processes. AIChE Journal, 1, 289-295.
https://doi.org/10.1002/aic.690010303
[14]  Chigier, N. and Farago, Z. (1992) Morphological Classification of the Disintegration of Round Liquid Jets in a Coaxial Air Stream. Atomization Sprays, 2, 137-153.
https://doi.org/10.1615/AtomizSpr.v2.i2.50
[15]  Chigier, N. and Reitz, R.D. (1996) Regimes of Jet Breakup and Breakup Mechanisms (Physical Aspects). Recent Advances in Spray Combustion, 1, 109-135.
https://doi.org/10.2514/5.9781600866418.0109.0135
[16]  Rayleigh, L. (1878) On the Instabilities of Jets. Proceedings of the London Mathematical Society, s1-10, 4-13.
https://doi.org/10.1112/plms/s1-10.1.4
[17]  Dombrowski, N. and Johns, W.R. (1963) The Aerodynamic Instability and Disintegration of Viscous Liquid Sheets. Chemical Engineering Science, 18, 203-214.
https://doi.org/10.1016/0009-2509(63)85005-8
[18]  Adelburg, M. (1968) Mean Drop Size Resulting from the Injection of a Liquid Jet into a High-Speed Gas Stream. AIAA Journal, 6, 1143-1147.
https://doi.org/10.2514/3.4686
[19]  Eroglu, H. and Chigier, N. (1991) Wave Characteristics of Liquid Jets from Airblast Coaxial Atomizers. Atomization Sprays, 1, 349-366.
https://doi.org/10.1615/AtomizSpr.v1.i4.10
[20]  Villermaux, E., Rehab, H. and Hopfinger, E.J. (1994) Breakup Régimes and Self-Sustained Pulsations in Coaxial Jets. Meccanica, 29, 393-401.
https://doi.org/10.1007/BF00987574
[21]  Porcheron, E., Carreau, J.L. and Le Visage, D. (2002) Effect of Injection Gas Density on Coaxial Liquid Jet Atomization. Atomization Sprays, 12, 209-227.
https://doi.org/10.1615/AtomizSpr.v12.i123.110
[22]  Leroux, B., Delabroy, O. and Lacas, F. (2007) Experimental Study of Coaxial Atomizers Scaling. Part I: Dense Core Zone. Atomization Sprays, 17, 381-407.
https://doi.org/10.1615/AtomizSpr.v17.i5.10
[23]  Seiner, J.M., Dash, S.M. and Kenzakowski, D.C. (2001) Historical Survey on Enhanced Mixing in Scramjet Engines. Journal of Propulsion and Power, 17, 1273-1286.
https://doi.org/10.2514/2.5876
[24]  Gutmark, E.J., Schadow, K.C. and Yu, K.H. (1995) Mixing Enhancement in Supersonic Free Shear Flows. Annual Review of Fluid Mechanics, 27, 375-417.
https://doi.org/10.1146/annurev.fl.27.010195.002111
[25]  Bogdanoff, D.W. (1994) Advanced Injection and Mixing Techniques for Scramjet Combustors. Journal of Propulsion and Power, 10, 183-190.
https://doi.org/10.2514/3.23728
[26]  Drozda, T.G., Baurle, R.A. and Drummond, J.P. (2016) Impact of Flight Enthalpy, Fuel Stimulant, and Chemical Reactions on the Mixing Characteristics of Several Injectors at Hypervelocity Flow Conditions. NASA Langley Research Center, Hampton, VA, Document ID: 20160009131.
https://ntrs.nasa.gov/api/citations/20160009131/downloads/20160009131.pdf
[27]  Menon, S. (1989) Shock-Wave-Induced Mixing Enhancement in Scramjet Combustors. 27th Aerospace Sciences Meeting, Reno, NV, 9-12 January 1989, AIAA Paper 89-0104.
https://doi.org/10.2514/6.1989-104
[28]  Ben-Yakar, A. and Hanson, R. (2001) Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview. Journal of Propulsion and Power, 17, 869-877.
https://doi.org/10.2514/2.5818
[29]  Hsu, K., Carter, C.D., Gruber, M.R. and Tam, C. (2009) Mixing Study of Strut Injectors in Supersonic Flows. 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Denver, CO, 2-5 August 2009, AIAA Paper 2009-5226.
https://doi.org/10.2514/6.2009-5226
[30]  Gu, H.B., Li, Z., Li, F., Chen, L.H., Gu, S.L., and Chang, X.Y. (2011) Characteristics of Supersonic Combustion with Hartmann-Sprenger Tube Aided Fuel Injection. 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Francisco, CA, 11-14 April 2011, AIAA Paper 2011-2326.
[31]  Solomon, J.T., Brown, K.A. and Brooks, K. (2020) Active Injection Nozzles for High-Speed Flow Mixing. AIAA Scitech 2020 Forum, Orlando, FL, 6-10 January 2020, AIAA Paper 2020-2245.
https://doi.org/10.2514/6.2020-2245
[32]  Uzun, A., Solomon, J.T., Foster, C.H., Oates, W.S., Hussaini, M.Y. and Alvi, F.S. (2013) Flow Physics of a Pulsed Microjet Actuator for High-Speed Flow Control. AIAA Journal, 51, 2894-2918.
https://doi.org/10.2514/1.J052525
[33]  Solomon, J.T., Foster, C. and Alvi, F.S. (2013) Design and Characterization of High-Bandwidth, Resonance Enhanced, Pulsed Microactuators: A Parametric Study. AIAA Journal, 51, 386-396.
https://doi.org/10.2514/1.J051806
[34]  Solomon, J.T., Cairnes, K., Nayak, C., Jones, M. and Alexander, D. (2018) Design and Characterization of Nozzle Injection Assemblies Integrated High-Frequency Microactuators. AIAA Journal, 56, 3436-3448.
https://doi.org/10.2514/1.J056642
[35]  Ali, M.Y., Arora, N., Topolski, M., Alvi, F.S. and Solomon, J.T. (2017) Properties of Resonance Enhanced Microjets in Supersonic Crossflow. AIAA Journal, 55, 1075-1081.
https://doi.org/10.2514/1.J055082
[36]  Solomon, J.T., Kumar, R. and Alvi, F.S. (2010) High-Bandwidth Pulsed Microactuators for High-Speed Flow Control. AIAA Journal, 48, 2386-2396.
https://doi.org/10.2514/1.J050405
[37]  Solomon, J.T. (2010) High-Bandwidth Unsteady Actuators for Active Control of High-Speed Flows. Ph.D. Dissertation, Florida State University, Florida.

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