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Information × Registration Number 0206U000042, 0103U004108 , R & D reports Title Development and improvement of gasdynamical calculation theoretical method for modern aviation gasturbine engines and their convertation in the surface power plant popup.stage_title Head Ludmila Boyko, Registration Date 06-01-2006 Organization National Aerospace University named by N.E.Zhukovsky "Kharkov aviation institute" popup.description2 Сalculation method of the centrifugal compressor stage features is presented. Mathematical model of the turbo-shaft aircraft engine whith a termwise description of rotating blades and stationary vanes of axial compressor is offered. Research of unsteady ratings of turbomachine working is directed on use in accounting methods and the condition running partial element in the usages process checking . Product Description popup.authors popup.nrat_date 2020-04-02 Close