Design Specification 1
✍️Calculations: Body and wings
Calculate a 3D model of the aircraft in the following conditions:
Attack angle, α: 0 / 2 / 4 degrees
Speed, V: 150 km/h
Define parameters as follows:
Ascensional force (general and distributed across the aircraft elements), kg;
resistance (general and distributed across the aircraft elements), kg;
wing/drag ratio.
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Specify the modeling environment used
Download the 3D model specifications: https://disk.yandex.ru/d/JS3gwl30wuGppQ
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