Regarding airfoil motion #254
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tolstoydebbarma
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Hi, for a static flapping airfoil (static = does not move in space except the flapping). ubcx=ubcy=ubcz=0 as the airfoil is static. My advice would be to start with the cylinder test case, replace the cylinder by a NACA profile and then make it flap. |
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Hi all, I want to simulate an airfoil NACA 0012 in Incompact3d. I want to give flapping motion to the trailing edge of the airfoil.
Do I need to change this subroutine? If I give ubcx = -0.5, ubcy = 0 and ubcz =0, what will be the next step?
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