What geometrical features of a lifting surface apart from which airfoil it has, I mean the ones visible from the top and front view of a wing (for ex: its span, AR, sweep, dihedral etc.) effects its lift coefficient and in what way? Also its stall characteristics.
I'm not looking for how these features change the total lift a wing produces but its effects on the wings lift coefficient, please correct me if I'm wrong and Cl is only for airfoils.
Edit: I ve found this which explains AR and sweep but how dihedral, anhedral or any other wing modification effects Cl still remains as a question.