Hydrogen-fueled detonation ramjet model: Wind tunnel tests at approach air stream Mach number 5.7 and stagnation temperature 1500 K
| Autor: | Frolov, S.M., Zvegintsev, V.I., Ivanov, V.S., Aksenov, V.S., Shamshin, I.O., Vnuchkov, D.A., Nalivaichenko, D.G., Berlin, A.A., Fomin, V.M., Shiplyuk, A.N., Yakovlev, N.N. |
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| Zdroj: | In International Journal of Hydrogen Energy 12 April 2018 43(15):7515-7524 |
| Databáze: | ScienceDirect |
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