Demonstrator of continuous-detonation air-breathing ramjet: Wind tunnel data


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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.

Sobre autores

S. Frolov

Semenov Institute of Chemical Physics; MIFI National Research Nuclear University

Autor responsável pela correspondência
Email: smfrol@chph.ras.ru
Rússia, Moscow, 119991; Moscow, 115409

V. Zvegintsev

MIFI National Research Nuclear University

Email: smfrol@chph.ras.ru
Rússia, Moscow, 115409

V. Ivanov

Semenov Institute of Chemical Physics

Email: smfrol@chph.ras.ru
Rússia, Moscow, 119991

V. Aksenov

Semenov Institute of Chemical Physics; MIFI National Research Nuclear University

Email: smfrol@chph.ras.ru
Rússia, Moscow, 119991; Moscow, 115409

I. Shamshin

Semenov Institute of Chemical Physics; MIFI National Research Nuclear University

Email: smfrol@chph.ras.ru
Rússia, Moscow, 119991; Moscow, 115409

D. Vnuchkov

Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch

Email: smfrol@chph.ras.ru
Rússia, Novosibirsk, 630090

D. Nalivaichenko

Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch

Email: smfrol@chph.ras.ru
Rússia, Novosibirsk, 630090

A. Berlin

Semenov Institute of Chemical Physics

Email: smfrol@chph.ras.ru
Rússia, Moscow, 119991

V. Fomin

Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch

Email: smfrol@chph.ras.ru
Rússia, Novosibirsk, 630090

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