hi. i have a doubt. Which configuration is more advantageous to the wings in terms of lift generated and stability? 1. a wing with a full span dihedral from fuselage to the tip 2. A wing with a partial span range dihedral from tips to somewhere in the wings and then straight till fuselage 3. a wing with a partial span dihedral from fuselage to some point on wing and then straight wings till the tip. please help if anyone knows.