Enter the Airfoil ID. This script will retrieve the parameters for the selected airfoil ID and draw the corresponding profile as a B-Spline curve.
This work has received funding from Nazarbayev University Grant No. 090118FD5328: "Shape Optimization of Lift and Thrust generating surfaces with the aid of IsoGeometric Analysis (SOLTIGA)". Disclaimer: This is a draft version of the database and errors may still be present.
