Visualization of Transient Ignition Flow-field in a 50 N Scale N2O/C2H5OH Thruster |
Kim, Dohun
(Department of Aerospace and Mechanical Engineering, Graduate School of Korea Aerospace University)
Park, Jaehyeon (School of Aerospace and Mechanical Engineering, Korea Aerospace University) Yu, Myunggon (School of Aerospace and Mechanical Engineering, Korea Aerospace University) Lee, Kyungeun (School of Aerospace and Mechanical Engineering, Korea Aerospace University) Koo, Jaye (School of Aerospace and Mechanical Engineering, Korea Aerospace University) |
1 | Bazarov, V., Yang, V. and Puri, P., Liquid Rocket Thrust Chambers: Aspect of Modeling, Analysis, and Design, American Institute of Aeronautics and Astronautics, Reston, VA, U.S.A., 2004. |
2 | Farago, Z. and Chigier, N., "Morphological Classification of Disintegration of Round Jets in a Coaxial Air Stream," Atomization and Sprays, Vol. 2, Issue 2, pp. 137-153, 1992. DOI |
3 | 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," Journal of Fluid Mechanics, Vol. 357, pp. 351-379, 1998. DOI ScienceOn |
4 | Varga, C.M., Lasheras, J.C. and Hopfinger, E.J., "Initial Breakup of a Small-diameter Liquid Jet by a High-speed Gas Stream," Journal of Fluid Mechanics, Vol. 497, pp. 405-434, 2003. DOI ScienceOn |
5 | 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. DOI ScienceOn |
6 | Branam, R. and Mayer, W., "Characterization of Cryogenic Injection at Supercritical Pressure," Journal of Propulsion and Power, Vol. 19, No. 3, pp. 342-355, 2003. DOI ScienceOn |
7 | Lux, J. and Haidn, O.J., "Flame Stabilization in High-Pressure Liquid Oxygen/Methane Rocket Engine Combustion," Journal of Propulsion and Power, Vol. 25, No. 1, pp. 15-23, 2009. DOI ScienceOn |
8 | Yang, B., Cuoco, F. and Oschwald, 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. DOI ScienceOn |
9 | Locke, J.M., Pal, S., Woodward, R.D. and Santoro, R.J., "High Speed Visualization of LOX/GH2 Rocket Injector Flowfield: Hot-Fire and Cold-Flow Experiments," 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Nashville, TN, U.S.A., AIAA 2010-7145, Jul. 2010. |
10 | Salgues, D., Mouis, A.G., Lee, S.Y., Kalitan, D., Pal, S. and Santoro, R.J., "Shear and Swirl Coaxial Injector Studies of LOX/GCH4 Rocket Combustion Using Non-Intrusive Laser Diagnostics," 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, U.S.A., AIAA 2006-757, Jul. 2006. |
11 | Cuoco, F., Yang, B., Bruno, C., Haidn, O.J. and Oschwald, M., "Experimental Investigation on LOx/CH4 Ignition," 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Fort Lauderdale, FL, U.S.A., AIAA 2004-4005, Jul. 2004. |