|August 27, 2014, 05:16||
How to calculate the AoA (Euler angles) in 6DOF model?
Join Date: Nov 2011
Posts: 8Rep Power: 5
Now I am simulating a case with sixDoF dynamic mesh model (similar to FOAM_TUTORIALS/incompressible/pimpleDyMFoam/wingMotion/wingMotion2D_pimpleDyMFoam).
During the post-process, all I want is the curves between Angle of Attack and lift coefficient. But I have no idea about how to calculate the AoA in this kind of aero-actuated model.
Does any one have any experiences?
|aoa, post-processing, sixdof|
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