Journal of the Korean Society of Propulsion Engineers ISSN:1226-6027(Print) 2288-4548(Online) 한국추진공학회지

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Schlieben, G., Kirchberger, C., Hupfer, A., Kau, H.-P., Soller, S. and Mäding, C., “Dynamic Characterization of Double Swirl Injectors for GOX/Kerosene,” 47^th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2011.

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Kalitan, D. M., Salgues, D., Mouis, A. G., Lee, S. Y., Pal, S. and Santoro, R. J., “Experimental Liquid Rocket Swirl Coaxial Injector Study Using Non-intrusive Optical Techniques,” 41^st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2005.

Huo, H., Wang, X. and Yang, V., “Several Fundamental Issues in Large Eddy Simulation of Supercritical Mixing and Combustion,” 52^nd Aerospace Sciences Meeting, 2014.

Carlanescu, R., Prisecaru, T., Prisecaru, M. and Soriga, L., “Swirl Injector for Premixed Combustion of Hydrogen-methane Mixtures,” Energy Resources Technology, Vol. 140, No. 7, pp. 1-9, 2018.

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Martinez-Sanchis, D., Sternin, A., Jocher, A. and Haidn, O., “Analysis of Turbulent Mixing in a Methane-oxygen Recessed Injector for Space Propulsion,” Physics of Fluids, Vol. 35, No. 7, 2023.

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Wang, X., Wang, Y. and Yang, V., “Geometric Effects on Liquid Oxygen/ Kerosene Bi-Swirl Injector Flow Dynamics at Supercritical Conditions,” AIAA Journal, Vol. 55, No. 10, pp. 1-9, 2017.

Kang, Y. H., Ahn, H. J., and Kim, J. S., “A Comparative Analysis for the Performance of 200 N-class Gaseous Methane-Liquid Oxygen Small Rocket Engine According to the Characteristic Length Variation,” Journal of the Korean Society of Propulsion Engineers, Vol. 24, No. 6, pp. 85-92, 2020.

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Ahn, H. J., Kang, Y. H. and Kim, J. S., “Spray Characteristics According to the Variation of Design Parameters and Gas-liquid Momentum-flux Ratio in a Swirl-coaxial Injector Applied to Small Rocket Engine,” Journal of the Korean Society of Propulsion Engineers, Vol. 27, No. 1, pp. 27-36, 2023.

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