1 |
Real-Time Plume Velocity Measurement of Solid Propellant Rocket Motors Using TDLAS Technique Song AC, Qin Z, Li JW, Li M, Huang K, Yang YJ, Wang NF Propellants Explosives Pyrotechnics, 46(4), 636, 2021 |
2 |
Insensitive High Explosives: V. Ballistic Properties and Vulnerability of Nitroguanidine Based Propellants Koch EC Propellants Explosives Pyrotechnics, 46(2), 174, 2021 |
3 |
Real-Time Plume Velocity Measurement of Solid Propellant Rocket Motors Using TDLAS Technique Song AC, Qin Z, Li JW, Li M, Huang K, Yang YJ, Wang NF Propellants Explosives Pyrotechnics, 46(4), 636, 2021 |
4 |
Insensitive High Explosives: V. Ballistic Properties and Vulnerability of Nitroguanidine Based Propellants Koch EC Propellants Explosives Pyrotechnics, 46(2), 174, 2021 |
5 |
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 |
6 |
Hypergolic ignition delay studies of solidified ethanol fuel with hydrogen peroxide for hybrid rockets John J, Nandagopalan P, Baek SW, Cho SJ Combustion and Flame, 212, 205, 2020 |
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Radiation heat transfer in ablating boundary layer combustion theory used for hybrid rocket motor analysis Budzinski K, Aphale SS, Ismael EK, Surina G, DesJardin PE Combustion and Flame, 217, 248, 2020 |
8 |
Agglomeration and combustion characteristics of solid composite propellants containing aluminum-based alloys Ao W, Fan ZM, Liu L, An YX, Ren JR, Zhao MT, Liu PJ, Li LKB Combustion and Flame, 220, 288, 2020 |
9 |
' 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 |
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Extended Eddy-Dissipation Model for Modeling Hydrogen Rocket Combustors Zhukov VP Combustion Science and Technology, 192(3), 531, 2020 |