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Information × Registration Number 0213U001314, 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 28-01-2013 Organization National aerospase university Kharkiv Aviation Institute popup.description2 Calculation method algorithm of operation characteristics of high-temperature gas-turbine engine, which is founded blade rows description of work operation in compressor and turbine is developed. Also calculation method algorithms of characteristics of the transonic axial turbine stage and the high-pressure centrifugal compressor stage are created. 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. № 0213U001314
1 documents found

Updated: 2026-03-26


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