| 1 |
ATOMIZATION AND DISTRIBUTION OF DROPLETS IN GAS-LIQUID SPRAYS BY COAXIAL SWIRL INJECTORS
Jeong G, Lee Y, Yoon J, Jo H, Yoon Y
Atomization and Sprays, 30(8), 607, 2020 |
| 2 |
Chemical Mechanism of MMH/NTO and Simulation in a Small Liquid Rocket Engine
Hou LY, Fu PF, Ba YT
Combustion Science and Technology, 191(12), 2208, 2019 |
| 3 |
The impacts of three flamelet burning regimes in nonlinear combustion dynamics
Nguyen TM, Sirignano WA
Combustion and Flame, 195, 170, 2018 |
| 4 |
A STUDY ON DISCHARGE COEFFICIENTS OF CLOSED-TYPE SWIRL INJECTORS FOR A LIQUID ROCKET ENGINE
Ahn K, Choi HS
Atomization and Sprays, 27(7), 569, 2017 |
| 5 |
AN EXTENSIVE STUDY ON THE DISCHARGE COEFFICIENTS OF OPEN-TYPE SWIRL INJECTORS
Ahn K, Choi HS
Atomization and Sprays, 27(10), 835, 2017 |
| 6 |
A PARAMETRICAL STUDY OF THE BREAKUP AND ATOMIZATION PROCESS OF TWO IMPINGING LIQUID JETS
Ruan C, Xing F, Huang Y, Xu LL, Lu XC
Atomization and Sprays, 27(12), 1025, 2017 |
| 7 |
Experimental proof of Zel'dovich cycle efficiency gain over cycle with constant pressure combustion for hydrogen-oxygen fuel mixture
Frolov SM, Aksenov VS, Ivanov VS
International Journal of Hydrogen Energy, 40(21), 6970, 2015 |
| 8 |
CFD analysis of transcritical methane in rocket engine cooling channels
Pizzarelli M, Nasuti F, Onofri M
Journal of Supercritical Fluids, 62, 79, 2012 |
| 9 |
Numerical investigation of combustion with non-gray thermal radiation and soot formation effect in a liquid rocket engine
Byun D, Baek SW
International Journal of Heat and Mass Transfer, 50(3-4), 412, 2007 |
