Author:
Migalin K V,Egorov A G,Sidenko K A
Abstract
Abstract
The results of the development of a new generation pulsating engine – an ejector dual-circuit PuVRD capable of under certain conditions going into detonation combustion mode are presented. It is assumed that in the engines of this type, having a double bend duct, the transition to detonation combustion is performed by precessing vortex core separation zone. The possible cause of the failure of the self-oscillating process during the transition to detonation combustion mode is analyzed.
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