Demonstrator of continuous-detonation air-breathing ramjet: Wind tunnel data |
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| Authors: | S. M. Frolov V. I. Zvegintsev V. S. Ivanov V. S. Aksenov I. O. Shamshin D. A. Vnuchkov D. G. Nalivaichenko A. A. Berlin V. M. Fomin |
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| Affiliation: | 1.Semenov Institute of Chemical Physics,Russian Academy of Sciences,Moscow,Russia;2.MIFI National Research Nuclear University,Moscow,Russia;3.Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch,Russian Academy of Sciences,Novosibirsk,Russia |
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| Abstract: | First experimental investigations were carried out into the detonation combustion of hydrogen in a demonstrator of an original-design air-breathing ramjet while blowing with an air flow at Mach 4 to 8 in an impulse wind tunnel, and for the first time under these conditions, continuous spin and longitudinal pulsed modes of detonation combustion of hydrogen in an annular combustor were detected. |
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