Unsteadiness in a Ramjet Model
V. M. Levin1, V. N. Karasev1, L. L. Kartovitskii1, E. A. Krymov2, O. A. Skachkov2
1Moscow Aviation Institute, 125993 Moscow
2Central Research Institute of Ferrous Metallurgy Bardin, 105005 Moscow
Keywords: ramjet, two-section combustor, aviation kerosene, working process, instability
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.
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