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How to calculate the AoA (Euler angles) in 6DOF model?

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Old   August 27, 2014, 05:16
Default How to calculate the AoA (Euler angles) in 6DOF model?
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Cheng Jie
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Hi Foamers,

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?

Jie
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