Titlebook: Information Technologies in the Design of Aerospace Engineering; Mykola Nechyporuk,Volodymyr Pavlikov,Dmytro Krytsk Book 2024 The Editor(s

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Transport Category Aircraft Fuselage Integrated Design,selage and increase the fuel efficiency of the aircraft by 6.4%, reduce the aerodynamic drag of the fuselage by 10%, increase the viewing angle from the cockpit by 10%. Fuselage nose, center and tail sections main parameters determination method is presented. Main theoretical characteristics for det

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