Airfoil Templates
- Althaus, Drella, Eppler, NACA, NASA Langley, NASA SC, Quabeck HQ and Selig airfoil families
- Aerodynamic characteristics of each airfoil:
- Lift coefficient (Cl)
- Drag coefficient (Cd)
- Pressure drag coefficient (Cdp)
- Preview of each airfoil
- Advanced search functionality based on user-defined ranges for the aerodynamic characteristics
- Direct import of selected airfoil into current sketch
Import NACA 0006 airfoil to the current sketch
Custom Templates
Templates are parameterized geometry models, useful for automatic re-designs. The templates can be dynamically created by the user.
This is an example of a wing where the wing span, the Leading Edge angle and the Ct are the parameters.
Example Parameterized Wing
User-imported templates are also supported.
Example of a fuselage template.