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