NACA4412 wing

Example simulation of a wing

Good agreement between the simulation and the experimental results is observed.

Vortex particle wake

As observed from the integrated loads the CL and CD compare favourably between the doublet and the vortex particle wake. The solution is not sensitive to the choice of a regularization kernel.



[1] Pinkerton, R. M. "Calculated and measured pressure distributions over the midspan section of the N.A.C.A 4412 airfoil", 1936

Last updated