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Hyoung Jin Lee
Hyoung Jin Lee
Inha University, Department of Aerospace Engineering
在 inha.ac.kr 的电子邮件经过验证
标题
引用次数
引用次数
年份
A flow visualization study on self-ignition of high pressure hydrogen gas released into a tube
YR Kim, HJ Lee, S Kim, IS Jeung
Proceedings of the Combustion institute 34 (2), 2057-2064, 2013
1462013
Experimental investigation on the self-ignition of pressurized hydrogen released by the failure of a rupture disk through tubes
HJ Lee, YR Kim, SH Kim, IS Jeung
Proceedings of the Combustion Institute 33 (2), 2351-2358, 2011
1112011
Robust HLLC Riemann solver with weighted average flux scheme for strong shock
SD Kim, BJ Lee, HJ Lee, IS Jeung
Journal of Computational Physics 228 (20), 7634-7642, 2009
1022009
Separation characteristics study of ridge-cut explosive bolts
J Lee, JH Han, YJ Lee, H Lee
Aerospace Science and Technology 39, 153-168, 2014
732014
Flow characteristics of small-sized supersonic inlets
HJ Lee, BJ Lee, SD Kim, IS Jeung
Journal of Propulsion and Power 27 (2), 306-318, 2011
632011
Numerical study on the spontaneous-ignition features of high-pressure hydrogen released through a tube with burst conditions
HJ Lee, JH Park, SD Kim, S Kim, IS Jeung
Proceedings of the Combustion Institute 35 (2), 2173-2180, 2015
562015
A parametric study of ridge-cut explosive bolts using hydrocodes
J Lee, JH Han, YJ Lee, H Lee
International Journal of Aeronautical and Space Sciences 16 (1), 50-63, 2015
522015
Effects of a wall on the self-ignition patterns and flame propagation of high-pressure hydrogen release through a tube
S Kim, HJ Lee, JH Park, IS Jeung
Proceedings of the Combustion Institute 34 (2), 2049-2056, 2013
392013
Performance analysis and mass estimation of a small-sized liquid rocket engine with electric-pump cycle
J Lee, TS Roh, H Huh, HJ Lee
International Journal of Aeronautical and Space Sciences 22, 94-107, 2021
352021
API5 confers cancer stem cell-like properties through the FGF2-NANOG axis
KH Song, H Cho, S Kim, HJ Lee, SJ Oh, SR Woo, SO Hong, HS Jang, ...
Oncogenesis 6 (1), e285-e285, 2017
342017
Realization of contact resolving approximate Riemann solvers for strong shock and expansion flows
SD Kim, BJ Lee, HJ Lee, IS Jeung, JY Choi
International journal for numerical methods in fluids 62 (10), 1107-1133, 2010
322010
Study on the combined effect of various injection conditions on the drag reduction by a counter-flow jet in supersonic flow
Y Kim, TS Roh, H Huh, HJ Lee
Aerospace Science and Technology 98, 105580, 2020
312020
Effect of opening area on the suppression of self-ignition of high-pressure hydrogen gas leaking in the air by an extension tube
SW Cha, TS Roh, HJ Lee
International Journal of Hydrogen Energy 46 (7), 5904-5915, 2021
282021
Development of a hybrid method in a 3-D numerical burn-back analysis for solid propellant grains
SH Oh, HJ Lee, TS Roh
Aerospace Science and Technology 106, 106103, 2020
232020
Drag reduction analysis of counterflow jets in a short penetration mode
J Lee, HJ Lee, H Huh
Aerospace Science and Technology 106, 106065, 2020
202020
Overseas research trends of an electric-pump cycle for application in upper-stage propulsion systems
W Ki, J Lee, H Lee, TS Roh, H Huh
Journal of the Korean Society of Propulsion Engineers 24 (1), 64-77, 2020
142020
Super-/hypersonic aero-optical effects induced by external jet cooling
S Lee, H Yoon, IS Jeung, HJ Lee, JK Lee
30th International Symposium on Shock Waves 1: ISSW30-Volume 1, 233-238, 2017
142017
Effects of opening conditions on the self-ignition of high pressurized hydrogen released through a tube
HJ Lee, SY Lee, JH Park, IS Jeung
25th ICDERS, Leeds, UK, 2015
142015
Development of ultra-low specific speed centrifugal pumps design method for small liquid rocket engines
HI Kim, TS Roh, H Huh, HJ Lee
Aerospace 9 (9), 477, 2022
132022
Development trend of liquid hydrogen-fueled rocket engines (part 1: performance and operation)
D Ha, TS Roh, H Huh, HJ Lee
International Journal of Aeronautical and Space Sciences 24 (1), 131-145, 2023
122023
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