
The uploaded files contain data for pressure, viscous and moment forces for 160 flow-through times generated for seven FFA-W3 airfoils between 21% and 50% thickness, and flat plate for 59 angles of attack between -180 and 180 degrees and Reynolds number of 10Million. Results of flow past a right circular cylinder has also been uploaded. The data can be used to extract polars, amplitude of load oscillations, and vortex shedding frequencies.
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