Use mathematical model for cad designing additional aerodynamic wing surfaces

Бесплатный доступ

In presented article formulated and justified method aided design using the developed software and mathematical model brought to the level application package by production costs for main aircraft, for maximum aerodynamic efficiency, for the specific type of main aircraft. The proposed method allows solving problem of determining the type and designing of required additional aerodynamic surface for, a specific main aircraft and giving economic interpretation solution.

Cad, additional aerodynamic surfaces, mathematical model, main aircraft

Короткий адрес: https://sciup.org/148202371

IDR: 148202371

Статья научная