Vidio in 8.26 flight[video]http://www.56.com/u41/v_NjI1NDY0NzA.html[/video]
Does any one know what benefit warping the wing serves?
An aircraft designer may also reduce the camber of the outboard section of the wings to increase the critical angle of attack (stall angle) at the wing tips
I can't imagine a J-20 without advanced TVC.
Wing warping was a technique used before the use of ailerons superseded it in the First World War. You might mean wing twist? This is reducing the angle of incidence at the wing tip profile compared with that of the root profile for reasons of not stalling the wing tip first, which is dangerous, and to reduce induced drag and possibly to do with supersonic flow I am ignorant about.Does any one know what benefit warping the wing serves?
I think j20 is designed to do without TVC. With it's canard configuration, super agility is still guarantee without TVC.