Here are all the basic information for your airfoil. The values are dynamic based on the modifications you make on the airfoil
You can make modifications on the airfoil by providing a scale, rotation and translation in the corresponding fields.
Then you can click on the "Modify original" button to apply your modifications on the original airfoil,
or click on the "Modify normalized" button to apply on a normalized version of the airfoil.
X point of rotation
Y point of rotation
%c x point of rotation
X-length of translation
Y-length of translation
%c x-length of translation
%c y-length of translation
How to use Airfoil Evaluator
Pick an airfoil from our database or upload one of your own
Make your modifications
Evaluate your airfoil
Automatic application of smoothing algorithms
Calculate the pressure distribution (CP)
Everything is downloadable!
Get an evaluation pdf report, a zip with all of the CP files, all the plots and coordinates