An Investigative Study of Gurney Flaps on a NACA 0036 Airfoil
This project examined 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...
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| Format: | Others |
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DigitalCommons@CalPoly
2011
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| Online Access: | https://digitalcommons.calpoly.edu/theses/524 https://digitalcommons.calpoly.edu/cgi/viewcontent.cgi?article=1554&context=theses |