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This article is cited in 1 scientific paper (total in 1 paper)
Control of thrust characteristics of a scramjet combustor with vibrational combustion using acoustic resonators
V. K. Baev, D. Yu. Moskvichev, A. V. Potapkin Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, 630090, Novosibirsk
Abstract:
The effect of a resonator on the thrust characteristics of a scramjet combustor with vibrational combustion of hydrogen is studied experimentally. A cylindrical tube with a confuser entrance was used as a combustion chamber. The centerline of the resonator is perpendicular to the combustor axis. It is shown that the thrust characteristics of the combustor depend on the resonator position relative to the combustor and on the linear dimensions of the resonator.
Received: 29.09.1999 Accepted: 04.03.2000
Citation:
V. K. Baev, D. Yu. Moskvichev, A. V. Potapkin, “Control of thrust characteristics of a scramjet combustor with vibrational combustion using acoustic resonators”, Fizika Goreniya i Vzryva, 36:5 (2000), 3–6; Combustion, Explosion and Shock Waves, 36:4 (2000), 553–556
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https://www.mathnet.ru/eng/fgv2233 https://www.mathnet.ru/eng/fgv/v36/i5/p3
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