화학공학소재연구정보센터
검색결과 : 7건
No. Article
1 ' 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
2 Hydrogen-fueled detonation ramjet model: Wind tunnel tests at approach air stream Mach number 5.7 and stagnation temperature 1500 K
Frolov SM, Zvegintsev VI, Ivanov VS, Aksenov VS, Shamshin IO, Vnuchkov DA, Nalivaichenko DG, Berlin AA, Fomin VM, Shiplyuk AN, Yakovlev NN
International Journal of Hydrogen Energy, 43(15), 7515, 2018
3 Continuous detonation combustion of ternary "hydrogen-liquid propane-air" mixture in annular combustor
Frolov SM, Aksenov VS, Ivanov VS, Shamshin IO
International Journal of Hydrogen Energy, 42(26), 16808, 2017
4 Wind tunnel tests of a hydrogen-fueled detonation ramjet model at approach air stream Mach numbers from 4 to 8
Frolov SM, Zuegintsev VI, Ivanov VS, Aksenov VS, Shamshin IO, Vnuchkov DA, Nalivaichenko DG, Berlin AA, Fomin VM
International Journal of Hydrogen Energy, 42(40), 25401, 2017
5 Experimental and computational studies of shock wave-to-bubbly water momentum transfer
Frolov SM, Avdeev KA, Aksenov VS, Borisov AA, Frolov FS, Shamshin IO, Tukhvatullinab RR, Basara B, Edelbauer W, Pachler K
International Journal of Multiphase Flow, 92, 20, 2017
6 Large-scale hydrogen-air continuous detonation combustor
Frolov SM, Aksenov VS, Lvanov VS, Shamshin IO
International Journal of Hydrogen Energy, 40(3), 1616, 2015
7 Reactive shock and detonation propagation in U-bend tubes
Frolov SM, Aksenov VS, Shamshin IO
Journal of Loss Prevention in The Process Industries, 20(4-6), 501, 2007