A DNS study of ignition characteristics of a lean iso-octane/air mixture under HCCI and SACI conditions CS Yoo, Z Luo, T Lu, H Kim, JH Chen proceedings of combustion institute 34 (2), 2985-2993, 2013 | 162 | 2013 |
Acoustic tuning of gas–liquid scheme injectors for acoustic damping in a combustion chamber of a liquid rocket engine CH Sohn, IS Park, SK Kim, HJ Kim Journal of sound and vibration 304 (3-5), 793-810, 2007 | 52 | 2007 |
Finite element analysis for acoustic characteristics of combustion stabilization devices SK Kim, HS Choi, HJ Kim, YS Ko, CH Sohn Aerospace Science and Technology 42, 229-240, 2015 | 37 | 2015 |
Development of analysis code for evaluation of acoustic stability of rocket engine combustor with various designs SK Kim, HJ Kim, CH Sohn Journal of the Korean Society for Aeronautical & Space Sciences 32 (6), 110-116, 2004 | 37* | 2004 |
Acoustic tests on atmospheric condition in a liquid rocket engine chamber YS Ko, K Lee, HJ Kim Transactions of the Korean Society of Mechanical Engineers B 28 (1), 16-23, 2004 | 28* | 2004 |
Experimental verification for acoustic damping enhancement by gaps in injector-formed baffles KJ Lee, HJ Kim, S Seo, HS Choi Journal of Propulsion and Power 25 (2), 435-442, 2009 | 27 | 2009 |
Geometric and number effect on damping capacity of Helmholtz resonators in a model chamber HJ Kim, JP Cha, JK Song, YS Ko Journal of sound and vibration 329 (16), 3266-3279, 2010 | 24 | 2010 |
Evaluation of the damping capacity according to the geometric and the number of resonator with thermal environment using a Rijke tube S Jo, Y Choi, HJ Kim Aerospace Science and Technology 88, 1-8, 2019 | 23 | 2019 |
Effect of pressure on effectiveness of quenching meshes in transmitting hydrogen combustion SY Yang, SH Chung, HJ Kim Nuclear engineering and design 224 (2), 199-206, 2003 | 22 | 2003 |
Acoustic damping enhanced by gaps in baffled injectors in an acoustic chamber IS Park, CH Sohn, HJ Kim Journal of Sound and Vibration 330 (12), 2747-2757, 2011 | 21 | 2011 |
Acoustic stability analysis of liquid propellant rocket combustion chambers SK Kim, H Kim, W Seol, C Sohn 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 4142, 2004 | 21 | 2004 |
Stability rating tests for the length-optimization of baffles in a liquid propellant combustion chamber using a pulse gun HJ Kim, S Seo, KJ Lee, YM Han, SY Lee, YS Ko Aerospace science and technology 12 (3), 214-222, 2008 | 18 | 2008 |
Numerical calculation of minimum ignition energy for hydrogen and methane fuels HJ Kim, SH Chung, CH Sohn KSME international journal 18, 838-846, 2004 | 18 | 2004 |
Acoustic Analysis for Design Optimization of Hub-Blade Baffle in Liquid Rocket Engine HJ Kim, SK Kim, WS Seol Transactions of the Korean Society of Mechanical Engineers B 28 (8), 945-952, 2004 | 18* | 2004 |
A numerical study on flow and heat transfer characteristics of supersonic second throat exhaust diffuser for high altitude simulation K Yim, H Kim, S Kim Journal of the Korean Society of Propulsion Engineers 18 (5), 70-78, 2014 | 17* | 2014 |
Film cooling effects on wall heat flux of a liquid propellant combustion chamber JG Kim, KJ Lee, S Seo, YM Han, HJ Kim, HS Choi 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 5196, 2006 | 17 | 2006 |
Development of a Liquid Rocket Engine Fuel-Rich Gas Generator SH Seo, KB Ahn, BJ Lim, JG Kim, KJ Lee, IY Moon, YM Han, CS Ryu, ... Proceedings of the Korean Society of Propulsion Engineers Conference, 181-185, 2006 | 15* | 2006 |
A Thermal Analysis of Liquid Rocket Combustors using a Modelling of Film Cooling Performance HJ Kim, WK Cho, YW Moon Journal of the Korean Society of Propulsion Engineers 10 (4), 85-92, 2006 | 14* | 2006 |
Effects of the O/F Ratio on the Performance of a Low Thrust LOX/Methane Rocket Engine with an ElecPump-fed Cycle B Yu, HD Kwak, HJ Kim International Journal of Aeronautical and Space Sciences, 1-10, 2020 | 13 | 2020 |
A rail-temperature-prediction model considering meteorological conditions and the position of the sun SU Hong, HU Kim, NH Lim, KH Kim, H Kim, SJ Cho International Journal of Precision Engineering and Manufacturing 20, 337-346, 2019 | 13 | 2019 |