Data from the pressure measurement of a pitching airfoil NACA643418

The present experimental work is motivated by the need for additional insight into the vortex-induced vibrations (VIV) of airfoils at high angle of attack from an aerodynamic perspective. Airfoil NACA643418 is set to periodic pitching motion. This experimental dataset temporarily contains surface pressure measurements of a pitching airfoil with a mean angle of attack set at 170 degrees, pitching frequency of 2 Hz, and pitching amplitude of 1o degrees.