Modifying/Exporting Airfoil Data

After importing an airfoil, you can modify its thickness and/or camber. Click the "Modify..." button or select "Modify Airfoil..." from the Airfoil menu. Type a new thickness and/or camber in the box, and click OK. Both thickness and camber are always specified as percent of the chord, and adding your own percent symbol here is an error.

If you don't like the airfoil modification and want to go back to the original data you imported, select "Revert To Saved Airfoil" in the Airfoil menu.

If you want to save the current airfoil data (modified or not) in a new airfoil data file, select "Export Airfoil Data..." from the Airfoil menu. The data will be saved in a new plain text file with the name you specify.