Hi guys!!!
I am new to this forum and by reading the threads I realized there are alot of things i didn't know about aero-modeling. Thanks to you guys for all the superb posts
Here is my query. I am designing a low weight RC plan to carry a specific sized payloads. Weight and battery being the major constraints i am planning to use an airfoil shaped fuselage to reduce the drag to minimum for high efficiency. Using XFLR5 i experimented with alot of airfoils and finally interpolated two NACA airfoils to get an optimized airfoil in terms of Cl and Cd.
Now i Don't know how to export the airfoil coordinates in a .dat or excel file?
Help anyone???
I am new to this forum and by reading the threads I realized there are alot of things i didn't know about aero-modeling. Thanks to you guys for all the superb posts
Here is my query. I am designing a low weight RC plan to carry a specific sized payloads. Weight and battery being the major constraints i am planning to use an airfoil shaped fuselage to reduce the drag to minimum for high efficiency. Using XFLR5 i experimented with alot of airfoils and finally interpolated two NACA airfoils to get an optimized airfoil in terms of Cl and Cd.
Now i Don't know how to export the airfoil coordinates in a .dat or excel file?
Help anyone???
