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Information × Registration Number 0214U000185, 0112U002133 , R & D reports Title Development of gas-turbine engine gas-dynamic characteristics modeling method with the blade rows flow detailed description popup.stage_title Head Ludmila Boyko, Registration Date 22-01-2014 Organization National aerospase university Kharkiv Aviation Institute popup.description2 Calculation method of operation characteristics of turboshaft gas-turbine engine, which is founded of work operation in multistage compressor and turbine, is developed. Flow calculation blade rows description method of the transonic cooled turbine stage is developed and its verification is carried. Approach to consider spatiality impeller high pressure centrifugal compressor stage in the flow calculation in it for weight-average parameters is developed. Product Description popup.authors Баришева О.С. Бойко Л.Г. Дьомін О.Є. Кіслов О.В. Карпенко О.Л. Максимов Ю.П. Піжанкова Н.В. popup.nrat_date 2020-04-02 Close