Aerowerx
Well-Known Member
My build requires a 13% thick Clark Y. The "normal" Clark Y is 11.7% thick.
I just came across the Airfoil Tools web site., and thought others might find it useful. Besides a database of over 1600 airfoils, it includes an airfoil plotter where you can customize the thickness, camber, and chord length.
You can also plot out a template spread across multiple sheets of paper, so you don't need a large format printer. Verify the dimensions after printing, though. Everything is in metric, including the paper size. It may not print correctly on A size (8.5 x 11 inch) paper. There might be a way to change this on the plotter page, but I haven't found it yet.
I just came across the Airfoil Tools web site., and thought others might find it useful. Besides a database of over 1600 airfoils, it includes an airfoil plotter where you can customize the thickness, camber, and chord length.
You can also plot out a template spread across multiple sheets of paper, so you don't need a large format printer. Verify the dimensions after printing, though. Everything is in metric, including the paper size. It may not print correctly on A size (8.5 x 11 inch) paper. There might be a way to change this on the plotter page, but I haven't found it yet.
