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Experimental investigation of H$_2$ combustion and supersonic cooling in an annular channel
R. V. Albegov, V. A. Vinogradov, G. G. Zhadan, S. A. Kobyzhskii Moscow
Abstract:
Results are presented for an experimental investigation of H$_2$ combustion and cooling in a channel which simulates the intake and combustion chamber of a supersonic ram jet. Stable operation conditions were obtained for operating the intake and combustion chamber with various fuel distributions through the feed zones. The cooling rate and the combustion efficiency were determined at the chamber wall at varying flows in the channel.
Received: 22.08.1990
Citation:
R. V. Albegov, V. A. Vinogradov, G. G. Zhadan, S. A. Kobyzhskii, “Experimental investigation of H$_2$ combustion and supersonic cooling in an annular channel”, Fizika Goreniya i Vzryva, 27:6 (1991), 24–29; Combustion, Explosion and Shock Waves, 27:6 (1991), 669–674
Linking options:
https://www.mathnet.ru/eng/fgv3452 https://www.mathnet.ru/eng/fgv/v27/i6/p24
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