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본 연구실은 우주 시대에 발맞추어 항공우주산업의 세계적 경쟁력을 갖추기 위해 노력하고 있습니다.
주 연구 분야로는 ‘액체로켓엔진 인젝터, 가스터빈 연소기, 난류확산화염’ 등이 있습니다.
Recent Publications
Effects of slit geometric parameters on spray characteristics of double-slit pintle injector
Inho Kim, Ingyu Lee, Daewoong Shim, Eunkwang Lee, Youngbin Yoon
2025
Experimental Thermal and Fluid Science
Effect of the Flow Passage Area Ratio on a Double Slit-Type Pintle Injector
Ingyu Lee, Daewoong Shim, Inho Kim, Youngbin Yoon
2024
International Journal of Aeronautical and Space Sciences
Experimental Study of Spray and Combustion Characteristics in Gas-Centered Swirl Coaxial Injectors: Influence of Recess Ratio and Gas Swirl
Jungho Lee, Ingyu Lee, Seongphil Woo, Yeoungmin Han, Youngbin Yoon
2024
Aerospace, Vol. 11 (3), No. 209
Characteristics of spray and combustion in gas-centered swirl coaxial injector with varying gas nozzle diameter
Jungho Lee, Seongphil Woo, Ingyu Lee, Yeoungmin Han, Youngbin Yoon
2024
Acta Astronautica, Vol. 215
Flame Structure of GCH4/GOX Pintle Model Combustor with Wall Confinement
Dae Hwan Kim, Hyeontaek Jo, Subeom Heo, Youngbin Yoon
2024
Aerospace Science and Technology, Vol. 145
Spray characteristics of a multi-slit type throttleable pintle injector with different slit heights
Subeom Heo, Juhwan Jeong, Youngbin Yoon
2024
Acta Astronautica, Vol. 215, pp. 475-492
On the spatial characteristics of the flame transfer function for a GCH4-GO2 swirl coaxial flame
Hyeontaek Jo, Dae Hwan Kim, Jinhyun Bae, Youngbin Yoon
2024
Acta Astronautica, Vol. 214, pp. 261-276
Breakup mode of continuous-type liquid-liquid pintle injector
Ingyu Lee, Gijeong Jeong, Youngbin Yoon
2023
Experimental Thermal and Fluid Science, Vol. 149