검색결과 : 2건
| No. | Article |
|---|---|
| 1 |
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 |
| 2 |
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 |