RESEARCH PAPERS
Betts, E. and Frederick, R., "A historical systems study of liquid rocket engine throttling capabilities," 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. p. 6541, 2010.
10.2514/6.2010-6541Tani, H., Teramoto, S. and Okamoto, K.. "Effects of injector geometry on cryogenic shear coaxial jets at supercritical pressures," Journal of Propulsion and Power, Vol. 31, No. 3, pp. 883-888, 2015.
10.2514/1.B35530Glogowski, M. and Micci, M., "Shear coaxial injector spray characterization near the LOX post tip region," 31st Joint Propulsion Conference and Exhibit, p. 2552, 1995.
10.2514/6.1995-2552Song, J. and Sun, B., "Coupled heat transfer analysis of thrust chambers with recessed shear coaxial injectors, Acta Astronautica, Vol. 132, pp. 150-160, 2017.
10.1016/j.actaastro.2016.12.026Asakawa, H., Nanri, H., Masuda, I., Shinohara, R., Ishikawa, Y. and Sakaguchi, H., "Study on Combustion Characteristics of LOX/LNG (methane) Co-axial Type Injector under High Pressure Condition," 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016.
10.2514/6.2016-5078Lux, 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.
10.2514/1.37308Matthew, J., Casiano, J., Hulka, R. and Yang, V., "Liquid-Propellant Rocket Engine Throttling: A Comprehensive Review," Journal of Propulsion and Power, Vol. 26, No. 5, pp. 897-923, 2010.
10.2514/1.49791Wanhainen, J.P., Antl, R.J., Hannum, N.P. and Mansour, A.H., "Throttling characteristics of a hydrogen-oxygen, regeneratively cooled, pump-fed rocket engine," NASA TM X-1043, 1964.
Rachuk, V., Shostak, A., Dmitrenko, A., Goncharov, G., Hernandez, R., Starle, R. and Hulka. J. "Benchmark testing of an enhanced operability LO2/LH2 RD-0120 engine," 32nd Joint Propulsion Conference and Exhibit. p. 2609, 1996.
10.2514/6.1996-2609Sankar, S., Brena, A., De La Rosa, Isakovic, A. and Bachalo, W., "Liquid atomization by coaxial rocket injectors," 29th Aerospace Sciences Meeting. p. 691, 1991.
10.2514/6.1991-691PMC240947Hardalupas, 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.
10.2514/3.23795Zaller, M.M. and Klem, M.D., "Coaxial injector spray characterization using water/air as simulants," JANNAF Combustion Meeting. 1991.
Ferraro, M., Kujala, R., Thomas, J.L., Glogowski, M. and Micci, M., "Measurements of shear coaxial injector sprays-cold flow and hot fire experiments," 32nd Joint Propulsion Conference and Exhibit. p. 3028, 1996.
10.2514/6.1996-3028Littler, M.G., Risha, G.A., Moore, J.D., Yetter, R.A. and Boyer. J.E., "Development and Testing of Liquid Simulants," Journal of Propulsion and Power, Vol. 37, No. 4, pp. 517-527, 2021.
10.2514/1.B38130Rahman, S. and Santoro. R., "A review of coaxial gas/liquid spray experiments and correlations," 30th Joint Propulsion Conference and Exhibit. 1994.
10.2514/6.1994-2772Woodward, R., Pal, S., Farhangi, S. and Santoro, R., "LOX/GH2 shear coaxial injector atomization studies at large momentum flux ratios," 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, p. 5203, 2006.
10.2514/6.2006-5203Cox, Jr G., "Rocket engine injection element characterization," 24th Joint Propulsion Conference. 1988.
10.2514/6.1988-3135Salgues, D., Mouis, A.G., Lee, S.-Y., Kalitan, D., Pal, S. and Santoro, R., "Shear and Swirl Coaxial Injector Studies of LOX/GCH4 Rocket Combustion Using Non-Intrusive Laser Diagnostics," 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006.
10.2514/6.2006-757Otsu, N., "A threshold selection method from gray-level histograms," IEEE transactions on systems, man, and cybernetics, Vol. 9, No. 1, pp. 62-66, 1979.
10.1109/TSMC.1979.4310076Kang, C., Lee, S., Han, S., Lee, K., Jung, H., Choi, D. and Ahn, K., "Step-by-step Tests for Continuous Thrust Control Hot-firing Test," Journal of the Korean Society of Propulsion Engineers, Vol. 27, No. 1, pp. 58-67, 2023.
10.6108/KSPE.2023.27.1.058De Giorgi, M.G., Sciolti, A. and Ficarella, A., "Different combustion models applied to high pressure LOX/CH4 jet flames," Proceedings of the 4th European Conference for Aerospace Sciences Saint Petersburg, Russia. pp. 4-8, 2011.
10.2514/6.2011-3587De Giorgi, M.G., Sciolti, A. and Ficarella, A., "Comparisons between different combustion models for High pressure LOX/CH4 jet flames," 41st AIAA Fluid Dynamics Conference and Exhibit, p. 3587, 2011.
10.2514/6.2011-3587Markatosm, N.C., "The mathematical modelling of turbulent flows," Applied Mathematical Modelling, Vol. 10, No. 3, pp. 190-220, 1986.
10.1016/0307-904X(86)90045-4Singla, G., Scouflaire, P., Rolon, C., Candel, S., Zurbach, S. and Thomas, J.l., "Experiments and simulations of lox/ch4 combustion at high pressures," Proceedings of the Combustion Institute, Vol. 30, pp. 2921-2928, 2005.
10.1016/j.proci.2004.08.063Giorgi, M.D., Sciolti, A. and Ficarella, A., "Application and Comparison of Different Combustion Models of High Pressure LOX/CH4 Jet Flames," Energies, Vol. 7, No. 1, pp. 477-497, 2014.
10.3390/en7010477- Publisher :The Korean Society of Propulsion Engineers
- Publisher(Ko) :한국추진공학회
- Journal Title :Journal of the Korean Society of Propulsion Engineers
- Journal Title(Ko) :한국추진공학회지
- Volume : 29
- No :1
- Pages :17-30
- Received Date : 2024-10-23
- Revised Date : 2024-12-09
- Accepted Date : 2025-01-05
- DOI :https://doi.org/10.6108/KSPE.2025.29.1.017
Journal of the Korean Society of Propulsion Engineers
