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Showing 1 to 1 of 1 for “"NACA 0036"”.
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An Investigative Study of Gurney Flaps on a NACA 0036 Airfoil
… the effect of Gurney flaps on a 2D, 2-ft chord NACA 0036 airfoil in the Cal Poly 3’x4’ low speed wind tunnel at 25 m/s. It also covered the numerical simulation of the experiment in computational fluid dynamics (CFD). During the study, problems with the wind tunnel data were seen. After a …