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Information × Registration Number 0215U006169, 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 10-03-2015 Organization National aerospase university Kharkiv Aviation Institute popup.description2 Calculation method of turboshaft engine operation characteristics was developed. This method is founded on mathematical model of gas turbine engine (GTE) which takes into account geometrical parameters of blade rows in axial multistage compressor and cooled turbine. The approach to aviation GTE mixing chamber calculation which is based on using of empirical dependence of temperature mixing coefficient was performed. Calculation method of flow gasdynamic parameters in high pressure centrifugal compressor stage by weight-average parameters with blade row profiling was 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
R & D report
Development of gas-turbine engine gas-dynamic characteristics modeling method with the blade rows flow detailed description
Head: Ludmila Boyko. Development of gas-turbine engine gas-dynamic characteristics modeling method with the blade rows flow detailed description. (popup.stage: ). National aerospase university Kharkiv Aviation Institute. № 0215U006169
1 documents found

Updated: 2026-03-22


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