검색결과 : 7건
No. | Article |
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1 |
Implementation of heterogeneous detonation in a pulsed combustor - PDE model Alhussan K, Assad M, Penazkov O Combustion Science and Technology, 190(12), 2245, 2018 |
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 |
Shockless Explosion Combustion: An Innovative Way of Efficient Constant Volume Combustion in Gas Turbines Bobusch BC, Berndt P, Paschereit CO, Klein R Combustion Science and Technology, 186(10-11), 1680, 2014 |
5 |
Schlieren visualization of multicyclic flame acceleration process in valveless pulsed detonation combustors Shimo M, Heister SD Combustion Science and Technology, 180(9), 1613, 2008 |
6 |
Pulsed detonation engine processes: Experiments and simulations Tangirala VE, Dean AJ, Chapin DM, Pinard PF, Varatharajan B Combustion Science and Technology, 176(10), 1779, 2004 |
7 |
Propulsive performances of pulsed detonations Zitoun R, Desbordes D Combustion Science and Technology, 144(1-6), 93, 1999 |