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Objective: SIMULATING A FLOW OVER AN NACA AIRFOILIn this report, a flow over a NACA airfoil has been simulated at the different angle of attack. Our main aim was to determine and compare the drag force ( X-direction ) and the lifting force ( Y-direction ) on the airfoil at the different angle of attack ( 0,2,4,6,8,10).…

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