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Moongeun Hong
Moongeun Hong
Verified email at kari.re.kr
Title
Cited by
Cited by
Year
Experimental study on spray characteristics of gas-centered swirl coaxial injectors
J Jeon, M Hong, YM Han, SY Lee
762011
Characterization of phase detection optical probes for the measurement of the dispersed phase parameters in sprays
M Hong, A Cartellier, EJ Hopfinger
International Journal of multiphase flow 30 (6), 615-648, 2004
632004
Stability of a swirled liquid film entrained by a fast gas stream
JP Matas, M Hong, A Cartellier
Physics of fluids 26 (4), 2014
482014
Atomisation et mélange dans les jets coaxiaux liquide-gaz
M Hong
Grenoble INPG, 2003
392003
Atomization and mixing in coaxial injection
M Hong, A Cartellier, EJ Hopfinger
Proc. 4th Int. Conf. on Launcher Technology, Liège Belgique, 2002
362002
An analysis of fuel–oxidizer mixing and combustion induced by swirl coaxial jet injector with a model of gas–gas injection
YJ Kim, CH Sohn, M Hong, SY Lee
Aerospace Science and Technology 37, 37-47, 2014
332014
Discharge coefficient of pressure-swirl atomizers with low nozzle opening coefficients
M Hong, J Jeon, SY Lee
Journal of Propulsion and Power 28 (1), 213-218, 2012
282012
Unsteadiness of the internal flow in an effervescent atomizer nozzle
M Hong, BA Fleck, DS Nobes
Experiments in fluids 55, 1-15, 2014
162014
Technology trends in additively manufactured small rocket engines for launcher applications
KO Lee, B Lim, DJ Kim, M Hong, K Lee
Journal of the Korean Society of Propulsion Engineers 24 (2), 73-82, 2020
142020
A study of the internal two-phase flow in gas-centered swirl coaxial injectors
M Hong, JP Matas, S Marty, AH Cartellier, SY Lee, A Delon
8th International Conference on Multiphase Flow, ICMF 2013, Jeju, Korea, May …, 2013
112013
Experimental correction of combustion gas properties of AN-based composite solid propellants used for turbo-pump starter
M Hong
Aerospace science and technology 16 (1), 56-60, 2012
112012
A Study on the Force Balance of a Main Oxidizer shutoff Valve
JH Jeon, MG Hong, HJ Kim, SY Lee
Journal of the Korean Society for Aeronautical & Space Sciences 37 (8), 812-818, 2009
112009
Opening Characteristics of a Main Oxidizer Shut-off Valve
M Hong
Journal of the Korean Society for Aeronautical & Space Sciences 45 (11), 989-997, 2017
72017
Turbine Rotor-Pyrostarter Coupled Test for the Verification of Thermo-Structural Suitability of a Turbopump Turbine
E Jeong, SH Kang, M Hong, H Lee, SY Lee, J Kim
Journal of the Korean Society of Propulsion Engineers 18 (1), 65-72, 2014
72014
Study on the Improvement in Cv of a Main Oxidizer shut-off Valve
MG Hong
Aerospace Engineering and Technology 8 (2), 140-148, 2009
72009
Improvement of a Flow Coefficient for the Recirculation Chill-down Flow in a Main Oxidizer Shut-off Valve
M Hong
Journal of the Korean Society of Propulsion Engineers 21 (4), 89-95, 2017
52017
Spray characterization using optical probes: Feasability of drop velocity, size and concentration measurements
M Hong, AH Cartellier, EJ Hopfinger
2nd Japanese European Two-phase Flow Group meeting. Japan., Pas précisé, 2001
52001
Performance Characteristics of a Main Oxidizer Shutoff Valve for Liquid Rocket Engines
D Jeong, M Hong, S Han
Journal of the Korean Society of Propulsion Engineers 21 (4), 28-35, 2017
42017
Ignition Test of an Oxidizer Rich Preburner
IY Moon, IS Moon, JH Yoo, JH Jeon, SM Lee, MG Hong, SU Ha, SH Kang, ...
Proceedings of the Korean Society of Propulsion Engineers Conference, 869-872, 2011
42011
On the Force Balance of a Main Oxidizer Shutoff Valve
MG Hong, SY Lee
Proceedings of the Korean Society of Propulsion Engineers Conference, 14-17, 2008
42008
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