Three-dimensional FFA-W3 static airfoil data over 360-degree angles of attack

<p>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.</p>