- #1
jgeating
- 36
- 0
What do you think about the feasibility of adding leading edge slats to a hang glider in order to reduce the stall speed and increase the wing loading.
I've seen charts showing nearly a twofold increase in the achievable coefficient of lift because the angle of attack can go so much higher without stalling (assuming flaps are present).
I have been wondering if it would be possible to decrease the wing area of a hang glider so much to the point where it could be deployable and fit in a large backpack.
I've seen charts showing nearly a twofold increase in the achievable coefficient of lift because the angle of attack can go so much higher without stalling (assuming flaps are present).
I have been wondering if it would be possible to decrease the wing area of a hang glider so much to the point where it could be deployable and fit in a large backpack.