- #1
risha99
- 1
- 0
Hi. I am trying to find an estimate for the lift generated by a flapping wing. For this scenario, we can assume that the wing has an AoA ranging from -45 deg to 45 deg. Also, we can ignore the lift generated by the upstroke because, for this specific wing design, a majority of the lift is generated during the downstroke. Ideally, my goal is to find what flapping frequency the wing would have to operate at to achieve a required amount of lift. I am having trouble in finding where to start. If anyone has any suggestions or useful resources, that would be awesome.