Here we minimize the drag of a rectangular wing with an aspect ratio of 10 while varying the aerodynamic twist and angle of attack subject to a lift constraint.
OpenAeroStruct available here: [ Ссылка ]
![](https://i.ytimg.com/vi/4mMlaZeqEE8/maxresdefault.jpg)
Here we minimize the drag of a rectangular wing with an aspect ratio of 10 while varying the aerodynamic twist and angle of attack subject to a lift constraint.
OpenAeroStruct available here: [ Ссылка ]