Engineering, 07.04.2020 00:52 ChloeN8912
For the NACA 2412 airfoil, the lift coefficient and moment coefficient about the quarter-chord at β6β¦ angle of attack are β0.39 and β0.045, respectively. At 4β¦ angle of attack, these coefficients are 0.65 and β0.037, respectively.
Calculate the location of the aerodynamic center.
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For the NACA 2412 airfoil, the lift coefficient and moment coefficient about the quarter-chord at β6...
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