Dovetailing between aircraft and turboprop engines at the initial stage design
Автор: Grigoriev Vladimir, Zagrebelniy Artem, Kistenev Nikita, Prokaev Alexey
Журнал: Известия Самарского научного центра Российской академии наук @izvestiya-ssc
Рубрика: Механика и машиностроение
Статья в выпуске: 6-3 т.15, 2013 года.
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In this paper we consider the process of evaluating the aerodynamic characteristics of the lung and regional aircraft in relation to the problem of coordination of their with the output characteristics turboprop engine.
Start design, coordination, mathematical model, turboprop engine, aircraft
Короткий адрес: https://sciup.org/148202606
IDR: 148202606
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