- #1
agurvinder
- 23
- 0
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.
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.