Analysis and selection of the parametric profile of a powerplant engine for a light trainer aircraft

Autor: Loginov, Vasiliy, Ukrainets, Yevgeniy, Kravchenko, Igor, Yelansky, Аlexandr

Publikováno v: Eastern-European Journal of Enterprise Technologies; Том 1, № 1 (2019): Engineering technological systems; 59-68
Восточно-Европейский журнал передовых технологий; Том 1, № 1 (2019): Производственно-технологические системы; 59-68
Східно-Європейський журнал передових технологій; Том 1, № 1 (2019): Виробничо-технологічні системи; 59-68

The relevance of this study is predetermined by the improvement to the fuel efficiency of an aircraft and, as a consequence, by the reduced cost of the life cycle of an aircraft engine, which is part of a power assembly at the training aircraft the t

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=scientific_p::a02aa692a6c8ad6b27f40fb1a3039c72
http://journals.uran.ua/eejet/article/view/154310

АЭРОДИНАМИЧЕСКИЙ ОБЛИК ТРАНСПОРТНОГО САМОЛЁТА СХЕМЫ «ЛЕТАЮЩЕЕ КРЫЛО» БОЛЬШОГО УДЛИНЕНИЯ

Publikováno v: MECHANICS OF GYROSCOPIC SYSTEMS; No. 27 (2014); 84-92
Механика гироскопических систем; № 27 (2014); 84-92
Механіка гіроскопічних систем; № 27 (2014); 84-92

"Normal" aerodynamic scheme despite the fact that it has become the dominant in global aviation, in terms of aerodynamics is not ideal. To create a lifting force only wing is just necessary. All other elements of aircraft glider - fuselage , horizont

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=scientific_p::760927d6ebf92a64e5eb317b4c957445
http://mgsys.kpi.ua/article/view/38043