Use the thin-airfoil theory to find the center of pressure

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Reference no: EM13718480

Use the thin-airfoil theory to find the center of pressure (as a function of lift coefficient) and the moment coefficient about the aerodynamic center for the NACA 2412 and the NACA 4412?

Reference no: EM13718480

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Use the thin-airfoil theory to find the center of pressure : Use the thin-airfoil theory to find the center of pressure (as a function of lift coefficient) and the moment coefficient about the aerodynamic center for the NACA 2412 and the NACA 4412?

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