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 and DRA-2303 airfoils, but their 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.
I appreciate any help you can provide.
You can find excel coordinates from NASA here (thanks to NASA):
https://data.nasa.gov/dataset/Supercritical-Airfoil-Coordinates/4qcc-xbk5
Let me know if this works for you.
Dear kallath
Just write the name of aerofile in google for which you want coordinates. It will provide a notepad file consisting of all coordinates required. Then there is an option in solid works which plot geometery from coordinates. Usr that option and u will get exactly what u want.
Thankd
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