| 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 |
' Rocket Engine with Continuously Rotating Liquid-Film Detonation
Frolov SM, Shamshin IO, Aksenov VS, Gusev PA, Zelensky VA, Evstratov EV, Alymov MI
Combustion Science and Technology, 192(1), 144, 2020 |
| 3 |
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 |
| 4 |
Inverse heat transfer method applied to capacitively cooled rocket thrust chambers
Perakis N, Haidn OJ
International Journal of Heat and Mass Transfer, 131, 150, 2019 |
| 5 |
The impacts of three flamelet burning regimes in nonlinear combustion dynamics
Nguyen TM, Sirignano WA
Combustion and Flame, 195, 170, 2018 |
| 6 |
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 |
| 7 |
AN EXTENSIVE STUDY ON THE DISCHARGE COEFFICIENTS OF OPEN-TYPE SWIRL INJECTORS
Ahn K, Choi HS
Atomization and Sprays, 27(10), 835, 2017 |
| 8 |
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 |
| 9 |
Combustion Dynamics of an Extreme Fuel-Rich Throttleable Rocket Engine During Continuously Throttling Process
Cheng P, Li QL, Kang ZT, Zhang XQ
Combustion Science and Technology, 189(4), 717, 2017 |
| 10 |
Experimental investigations on H-2/air rotating detonation wave in the hollow chamber with Laval nozzle
Zhang HL, Liu WD, Liu SJ
International Journal of Hydrogen Energy, 42(5), 3363, 2017 |
