| 8 |
- Integrated Design of a Hybrid Sounding Rocket using Liquid N2O Oxidizer
- J.Y.Heo, M.G.Cho, H.J.Park, S.J.Kim, H.J.Moon, J.K.Kim, H.G.Sung
- Asia-Pacific International Symposium on Aerospace Technology (APISAT), Gifu, Japan, 11.4-6, 2009
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| 7 |
- Design of TSTO Reusable Launch Vehicle using oxygen collection system
- Hong-Gye Sung, Shikyung Yoon
- International Astronautical Federation (IAF), Daejeon, Korea, 10.14-15, 2009
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| 6 |
- Fluidic Thrust Vector Control of Supersonic Jet using Co-flow Injection
- Jun-Young Heo, Kwang-Hee Yoo, Yeol Lee, Hong-Gye Sung
- AIAA/ASME/SAE/ASEE Joint Propulsion, Denver, Colorado, USA, 8.2-5, 2009
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| 5 |
- Large Eddy Simulation of the Turbulent Flow Field in a Swirl Stabilized Annular Combustor
- J.C.Kim, H.G.Sung, D.K.Min, V.Yang
- American Institute of Aeronautics and Astronautics (AIAA), Florida, USA, 1.5-8, 2009
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| 4 |
- Flow Dynamics in a Supersonic Diffuser at Minimum Starting Condition to Simulatiote Rocket's High Altitude Test on the Ground
- Yeom, S.K.Yoon, H.G.Sung, Y.W.Kim, S.H.Oh
- Asian Joint Conference on Propulsion and Power (AJCPP), Gyeongju, Korea, 3.6-8, 2008
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| 3 |
- Study on Design- and Operation- Parameters of Supersonic Exhaust Diffusers
- H.G.Sung, S.K.Yoon, H.W.Yeom, J.K.Kim, Y.S.Ko, Y.W.Kim, S.H, Oh
- American Institute of Aeronautics and Astronautics (AIAA), Reno, Nevada, USA, 1.7-10, 2008
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| 2 |
- Large Eddy Simulation on the Lean Premixed Swirl Stabilized Combustor of LM6000
- J.C.Kim, H.G.Sung, B.J.Cha
- Jeju, Korea, 2008.
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| 1 |
- Numerical Investigation on Combustion Dynamics in a Swirl Stabilized Combustor
- Jong-Chan Kim, JaYe Koo, Hong-Gye Sung, DaeSung Lee, YongMin Jun
- Seoul, Korea , 2007
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Research