- #1
Keen
- 2
- 0
Hi,
I've been designing a wing lately, and have been trying to figure out something. Hope someone could help.
Considerations of small trim deflection have led to a design requirement of Cmac for the wing. I've been trying to figure out ways to reduce this to a Cmac value for the airfoil. In general, they are not the same.
Would anyone know of any ways?
Thanks very much.
I've been designing a wing lately, and have been trying to figure out something. Hope someone could help.
Considerations of small trim deflection have led to a design requirement of Cmac for the wing. I've been trying to figure out ways to reduce this to a Cmac value for the airfoil. In general, they are not the same.
Would anyone know of any ways?
Thanks very much.