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Information × Registration Number 0206U000014, 0103U004030 , R & D reports Title The complex-conjugate models of impulse heat machines popup.stage_title Head Ambrozewicz Alexandr, Registration Date 03-01-2006 Organization National Aerospace University named by N.E.Zhukovsky "Kharkov aviation institute" popup.description2 The universal technology of the lenient numerical researches has been developed and led to the level of the functioning specimens - two-stroke engine with crank-chamber blowing, bypass motor-compressor aerojet engine of small thrust (MC AJE ST) of the integral scheme and MC AJE ST of the block scheme with the drive of the displacement compressor from the serial two-stroke piston engine. The new way of the sheet materials fragmentation from aluminum alloys based on the combine (heat and power) effect of the high-temperature supersonic jet generated by researchable combustion chambers has been proposed. Product Description popup.authors popup.nrat_date 2020-04-02 Close