Regarding airfoil motion #254
-
|
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? |
Beta Was this translation helpful? Give feedback.
Answered by
slaizet
Feb 21, 2024
Replies: 1 comment
-
|
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. |
Beta Was this translation helpful? Give feedback.
0 replies
Answer selected by
mathrack
Sign up for free
to join this conversation on GitHub.
Already have an account?
Sign in to comment
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.
Best,
Sylvain