Two-surface canard aircraft cannot easily make effective use of flaps on the main wing to increase lift, due to the aft position of the wing trailing edge; thus the main wing size cannot be reduced effectively with flaps.
Thus the main wing size cannot be reduced effectively with flaps. Two-surface canard aircraft generally cannot make effective use of flaps on the main wing to increase lift.
Two-surface canard aircraft generally cannot make effective use of flaps on the main wing to increase lift. Thus the main wing size cannot be reduced effectively with flaps.
Two-surface canard aircraft generally cannot make effective use of flaps on the main wing to increase lift. Thus the main wing size cannot be reduced effectively with flaps.