ANSYS FLUENT - Tutorial Perfil NACA 2412 - NSIV.IO
ANSYS FLUENT - Tutorial Perfil NACA 2412 - NSIV.IO
Feb 20, 2022
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For the NACA 2412 airfoil, the lift coefficient and moment coefficient about the quarter-chord at -6^∘ angle of attack are -0.39 and -0.045, respectively. At 4^∘ angle of attack, these coefficients are 0.65 and -0.037, respectively. Calculate the location of the aerodynamic center. | Numerade
For the NACA 2412 airfoil, the lift coefficient and moment coefficien…
Nov 29, 2023
numerade.com
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