REDesigner09
Aerospace
- Nov 19, 2010
- 227
Hi,
This is in relation to the airfoil cross-section question I just posted. If the aligned or unfolded cross-section doesn't work, then perhaps, the local cross-section may work for what I am trying to present.
However, like the aligned or unfolded cross-section attempts, I couldn't quite get this to work.
What are your suggestions or steps to get this to work?
Thanks
This is in relation to the airfoil cross-section question I just posted. If the aligned or unfolded cross-section doesn't work, then perhaps, the local cross-section may work for what I am trying to present.
However, like the aligned or unfolded cross-section attempts, I couldn't quite get this to work.
What are your suggestions or steps to get this to work?
Thanks