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This article is cited in 2 scientific papers (total in 2 papers)
Unsteadiness in a ramjet model
V. M. Levina, V. N. Karaseva, L. L. Kartovitskiia, E. A. Krymovb, O. A. Skachkovb a Moscow Aviation Institute (National Research University), Moscow, 125993, Russia
b Bardin Central Research Institute of Ferrous Metallurgy, Moscow, 105005, Russia
Abstract:
The process of combustion of a hydrocarbon fuel in a pulsed mode is discussed on the basis of results of ramjet testing in an external flow modeling a Mach 5 flight.
Keywords:
ramjet, two-section combustor, aviation kerosene, working process, instability.
Received: 21.01.2013
Citation:
V. M. Levin, V. N. Karasev, L. L. Kartovitskii, E. A. Krymov, O. A. Skachkov, “Unsteadiness in a ramjet model”, Fizika Goreniya i Vzryva, 49:6 (2013), 68–75; Combustion, Explosion and Shock Waves, 49:6 (2013), 682–689
Linking options:
https://www.mathnet.ru/eng/fgv86 https://www.mathnet.ru/eng/fgv/v49/i6/p68
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