METHOD OF detonation regime burning in combustion chambers SUPERSONIC ramjet ENGINE

摘要

the way the u0434u0435u0442u043eu043du0430u0446u0438u043eu043du043du043eu0433u043e regime u0433u043eu0440u0435u043du0438u00a0 in u043fu0440u00a0u043cu043eu0442u043eu0447u043du043eu043c air jet engine for supersonic and / or u0433u0438u043fu0435u0440u0437u0432u0443u043au043eu0432u043eu0433u043e aircraft that next to fuel air gas mixture in the chamber u0441u0433u043eu0440u0430u043du0438u00a0 u0434u0432u0438u0433u0430u0442u0435u043bu00a0, generation of shock waves in the flow of the cell u0441u0433u043eu0440u0430u043du0438u00a0 produced re u0433u0443u043bu0438u0440u0443u0435u043cu044bu043cu0438 elements u0441u0433u043eu0440u0430u043du0438u00a0 cameras.for example, the system of the two flat symmetrical u043au043bu0438u043du044cu0435u0432, u0434u0435u0442u043eu043du0430u0446u0438u043eu043du043du043eu0435 combustion mixture in the cell u0441u0433u043eu0440u0430u043du0438u00a0 with subsequent expansion of detonation products in snot, exe u0438u0447u0430u044eu0449u0438u0439u0441u00a0 so that flow of the cell u0441u0433u043eu0440u0430u043du0438u00a0 a system of symmetrical inclined falling shock waves.in the central part of the transverse u0441u0435u0447u0435u043du0438u00a0 chamber u0441u0433u043eu0440u0430u043du0438u00a0 by u0432u0437u0430u0438u043cu043eu0434u0435u0439u0441u0442u0432u0438u00a0 these waves with each other u0444u043eu0440u043cu0438u0440u0443u0435u0442u0441u00a0 u043fu0435u0440u0435u0441u0436u0430u0442u0430u00a0 u0434u0435u0442u043eu043du0430u0446u0438u043eu043du043du0430u00a0 wave - leg maha, with the possibility of u0440u0435u0433u0443u043bu0438u0440u043eu0432u0430u043du0438u00a0 size and u043cu0435u0441u0442u043eu043fu043eu043bu043eu0436u0435u043du0438u00a0 in the running of the cell u0441u0433u043eu0440u0430u043du0438u00a0, which is mixed with the combustion u0434u0435u0442u043eu043du0430u0446u0438u043eu043du043du043eu0435 u0437u043eu0432u0430u043du0438u0435u043c for high temperature area of the detonation products.as well as u043du0430u0440u00a0u0434u0443 this u043eu0431u0440u0430u0437u0443u044eu0442u0441u00a0 tilt reflected shock waves between the leg and the walls of the maha cells without u0433u043eu0440u0435u043du0438u00a0 process, temperature of gas mixture for him and significantly less than in the area of the detonation products and the size of the feet, maha, and thus its position in the longitudinal direction of the camera u0441u0433u043eu0440u0430u043du0438u00a0,as well as its stationary process set by geometric parameters u0438u0437u043cu0435u043du0435u043du0438u00a0 regulatory elements u0441u0433u043eu0440u0430u043du0438u00a0 cameras depending on the number of the flow at mach the camera u0441u0433u043eu0440u0430u043du0438u00a0 and the chemical composition of the incoming fuel air gas mixture.