Technical Papers
May 4, 2017

Spray Patterns and Injection Characteristics of Gas-Centered Swirl Coaxial Injectors

Publication: Journal of Aerospace Engineering
Volume 30, Issue 5

Abstract

Spray characteristics of gas-centered swirl coaxial injectors, which are commonly used in staged combustion cycle engines, are investigated numerically and experimentally. The spray angle and the spreading angle are the quantitative parameters selected for experimental and numerical studies, respectively. Various gas/liquid Reynolds numbers are adopted for the operating conditions. For a fixed gas Reynolds number, the spreading angle increases with the liquid Reynolds number. Through the comparative study of the spray angle from water/air experiments, the spreading angle is analyzed for different momentum flux ratios (MFRs). The comparison of the spray and spreading angles for different MFRs shows good agreement. Modeling and study of gas–gas flow is a useful approach to understanding spray characteristics of gas–liquid flow.

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Acknowledgments

This work was supported by Advanced Research Center Program (NRF-2013R1A5A1073861) through the National Research Foundation of Korea (NRF) grant funded by the Korean government (MSIP) contracted through Advanced Space Propulsion Research Center at Seoul National University. The first author appreciates Dr. G. Jourdain for his assistance in writing the manuscript.

References

Culick, F. E. C., and Yang, V. (1995). “Overview of combustion instabilities in liquid-propellant rocket engines.” Liquid Rocket Engine Combustion Instability, 169, AIAA, Washington, DC, 3–38.
ESI Group. (2012). “CFD-ACE User’s manual Ver. 2012.” Paris.
Fukagata, K., Kasagi, N., Ua-Arayaporn, P., and Himeno, T. (2007). “Numerical simulation of gas-liquid two-phase flow and convective heat transfer in a micro tube.” Int. J. Heat Fluid Flow, 28(1), 72–82.
Hamid, A. H. A, and Atan, R. (2009). “Spray characteristics of jet-swirl nozzles for thrust chamber injector.” Aerosp. Sci. Tech., 13(4–5), 192–196.
Hong, Y. S. (2007). “Space propulsion.” Chung Moon Gak, Seoul.
Irannejad, A., and Jaberi, F. (2014). “Large eddy simulation of turbulent spray breakup and evaporation.” Int. J. Multiphase Flow, 61, 108–128.
Jeon, J., Hong, M., Han, Y. M., and Lee, S. Y. (2011). “Experimental study on spray characteristics of gas-centered swirl coaxial injectors.” J. Fluids Eng., 133(12), 1–7.
Jones, W. P., Lettieri, C., Marquis, A. J., and Navarro-Martinez, S. (2012). “Large eddy simulation of the two-phase flow in an experimental swirl-stabilized burner.” Int. J. Heat Fluid Flow, 38, 145–158.
Keller, J., Gebretsadik, M., Habisreuther, P., Turrini, F., Zarzalis, N., and Trimis, D. (2015). “Numerical and experimental investigation on droplet dynamics and dispersion of a jet engine injector.” Int. J. Multiphase Flow, 75, 144–162.
Kim, T. H., Kim, Y. M., and Kim, S. K. (2013). “Effects of pressure and inlet temperature on coaxial gaseous methane/liquid oxygen turbulent jet flame under transcritical conditions.” J. Supercrit. Fluids, 81, 164–174.
Kim, Y. J., Sohn, C. H., Hong, M. G., and Lee, S. Y. (2014). “An analysis of fuel-oxidizer mixing and combustion induced by swirl coaxial jet injector with a model of gas-gas injection.” Aerosp. Sci. Tech., 37, 37–47.
Launder, B. E., and Spalding, D. B. (1974). “The numerical computation of turbulent flows.” Comput. Meth. Appl. Mech. Eng., 3, 269–289.
Liu, J., Zhang, X. Q., Li, Q. L., and Wang, Z. G. (2013). “Effect of geometric parameters on the spray cone angle in the pressure swirl injector.” Proc. Instit. Mech. Eng., Part G: J. Aerosp. Eng., 227(2), 243–353.
Moon, S. S., Abo-Serie, E., and Bae, C. S. (2008). “The spray characteristics of a pressure-swirl injector with various exit plane tilts.” Int. J. Multiphase Flow, 34(7), 615–627.
Oefelein, J. C., and Yang, V. (2006). “Combustion science and technology special issue: Supercritical fluid transport and combustion.” Combust. Sci. Tech., 178(1–3), 1–621.
Park, K. J., Lee, J. Y., and Yoon, Y. B. (2015). “Study of gap thickness in gas-centered swirl coaxial injector.” Proc., KSPE spring conf. (in Korean), 450–453.
Poinsot, T., and Veynante, D. (2001). Theoretical and numerical combustion, R.T. Edwards, Philadelphia.
Richecoeur, F., Ducruix, S., Scouflaire, P., and Candel, S. (2008). “Experimental investigation of high-frequency combustion instabilities in liquid rocket engine.” Acta Astronaut., 62(1), 18–27.
Singla, G., Scouflaire, P., Rolon, J. C., and Candel, S. (2007). “Flame stabilization in high pressure LOx/GH2 and GCH4 combustion.” Proc. Combust. Inst., 31(2), 2215–2222.
Sohn, C. H., Kim, Y. J., Kim, Y. M., and Pikalov, V. P. (2012). “A scaling method for combustion stability rating of coaxial gas-liquid injectors in a subscale chamber.” J. Mech. Sci. Tech., 26(11), 3691–3699.
Sutton, G. P. (2003). “History of liquid-propellant rocket engines in Russia, formerly the Soviet Union.” J. Propul. Power, 19(6), 1008–1037.
Zong, N., and Yang, V. (2007). “Near-field flow and flame dynamics of LOX/methane shear-coaxial injector under supercritical conditions.” Proc. Combust. Inst., 31(2), 2309–2317.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 30Issue 5September 2017

History

Received: Aug 14, 2016
Accepted: Feb 1, 2017
Published online: May 4, 2017
Published in print: Sep 1, 2017
Discussion open until: Oct 4, 2017

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Authors

Affiliations

Graduate Student, Dept. of Mechanical Engineering, Sejong Univ., Seoul 143-747, Republic of Korea. E-mail: [email protected]
Chae Hoon Sohn [email protected]
Professor, Dept. of Mechanical Engineering, Sejong Univ., Seoul 143-747, Republic of Korea (corresponding author). E-mail: [email protected]
Gujeong Park [email protected]
Graduate Student, School of Mechanical and Aerospace Engineering, Seoul National Univ., Seoul 151-742, Republic of Korea. E-mail: [email protected]
Youngbin Yoon [email protected]
Professor, School of Mechanical and Aerospace Engineering, Seoul National Univ., Seoul 151-742, Republic of Korea. E-mail: [email protected]

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