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 |
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 |
| 4 |
Velocity fluctuation near the detonation limits Gao YA, Lee JHS, Ng HD Combustion and Flame, 161(11), 2982, 2014 |
| 5 |
High resolution WENO simulation of 3D detonation waves Wang C, Shu CW, Han WH, Ning JG Combustion and Flame, 160(2), 447, 2013 |
| 6 |
Numerical study of acoustic coupling in spinning detonation propagating in a circular tube Sugiyama Y, Matsuo A Combustion and Flame, 160(11), 2457, 2013 |
| 7 |
Transmission of near-limit detonation wave through a planar sudden expansion in a narrow channel Wu MH, Kuo WC Combustion and Flame, 159(11), 3414, 2012 |