- #1
cosmic time
- 9
- 0
When an air passes over the wingtip of the airfoil, the upwash created at the leading edge 'reduces' the Angle of Attack, thus reducing lift. So why does this affect increase induced drag. The way I understand it, the greater the AoA (more lift), the more induced drag that is generated.
Help would be appreciated,
thank you.
Help would be appreciated,
thank you.