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Amruthwo's interactive graph and data of "Lift Coefficient vs Angle of Attack [NACA 2415]" is a scatter chart, showing Experimental, CFD, Theoretical; with Angle of Attack (Degrees) in the x-axis and Lift Coefficient, Cl in the y-axis.. The x-axis shows values from -22.669427826353736 to 26.669427826353736. The y-axis shows values from -2.233515824611111 to 3.127748727611111.