[Dronzer]

Hi all,

I hope you all are doing well.
I am working on the simulation of airfoils with boundary layer suction.
I found a reference to validate my CFD results, as shown below.

"Stanewsky E, Délery J, Fulker J, de Matteis P, editors. Drag Reduction by Shock and Boundary Layer Control: Results of the Project EUROSHOCK II. Supported by the European Union 1996-1999. Springer Science & Business Media; 2002 Apr 24."

They used RAE 5225 airfoil, but its coordinates were not given explicitly.
Kindly share it with me if anybody has the coordinates.

Also, please feel free to suggest any other references which contain detailed experimental data of boundary layer suction on airfoil shapes.

Thanks in advance.