reviewnaca 0012 experimental dataShare on FacebookShare on Twitter223IMAGESNaca 0012NACA 0012 AirfoilNACA 0012 AirfoilNaca 0012 airfoilNACA 0012, M∞ = 0.15, Re = 6 × 10 6 , drag polar: comparison with...Solved Experimental data for the NACA 0012 airfoil is shown
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