SCHEME OF HYDROGEN IGNITION IN DUCT WITH SHOCK WAVES
0000-0002-3259-8567 The material was received by the Editorial Board: 24.04.2014
In article results of the analysis of processes of self-ignition and combustion propagation are given in the multi-injector combustion chamber with high supersonic speeds of an air flow. It is established that fuel ignition at high Mach numbers, bringing to flame propagation on all volume of combustor and combustion stabilization, happens not in recirculation area behind a step, and in the field of interaction of shock waves with an boundary layer on walls or behind this area downstream near an angular point of the combustion chamber. The scheme of development of process of combustion in the combustion chamber with significantly three-dimensional configuration is in details considered. Keywords:
hydrogen ignition, supersonic speeds, shock waves, combustion stabilization.
УДК 533.6.011.5; 533.6.072
SCHEME OF HYDROGEN IGNITION IN DUCT WITH SHOCK WAVES References: Goldfeld M. A., Starov A. V. SCHEME OF HYDROGEN IGNITION IN DUCT WITH SHOCK WAVES . Vestnik NSU. Series: Physics. 2014, vol. 9, no. 2. P. 116–127 (in Russ.). DOI: 10.54362/1818-7919-2014-9-2-116-127