Curve Fitting in Design Modeller
Can anyone advise the best way to import aerofoil point data to generate curves using Ansys Design Modeller that produces a cleaner trailing edge as its causing me issues with me inflation layer?
RAE5225 transonic aerofoil point data attached.
Images of point data plotted in Excel.
Any questions or should I need to provide additional data please do not hesitate to let me know.