OpenFOAM Aircraft dynamic meshing
 

Hello Every one,

Consider me a rookie in OpenFoam.

I would like to ask a basic few questions. I have read many threads but could not find an accurate answer to my doubts.

I would like to carry out coning motion of an aircraft. My intention is to rotate the rigid body about the X axis at a constant Omega and get the transient results for CL, CM, CN etc..

How can I go about this problem? Which tutorials should I be focused on?

Many thanks for the help in advance.


Regards
Shereez