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Information × Registration Number 0209U005790, 0106U001048 , R & D reports Title Theoretical bases of blade machines mathematical models development for the modern gasturbine engines and gas-compressor units and building the high level engines on the models's base popup.stage_title Head Ludmila Boyko, Registration Date 31-03-2009 Organization National Aerospace University named by N.E.Zhukovsky "Kharkov aviation institute" popup.description2 A turboshaft engine performances computation method taking into account terms of work and the geometrical parameters of multistage axial compressor blades, air bleeding from the running part of compressor is developed. A method of decision of flow structure and total behaviors of axial-radial centrifugal compressor stage with rotor blades having the spatial profiling is created. Product Description popup.authors popup.nrat_date 2020-04-02 Close