Hello,

I am trying to compute the deformation of a 3D wing in a flow. To do so, I firstly ran a CFD computation on my wing. It allowed me to have the pressure and the viscous stress on the fin. After I defined a 3D model in Abaqus, meshed with C3D8R elements. The goal is to apply on this model the pressure and the viscous stress computed earlier and then check the deformations.

I see how to apply a non-uniform pressure in Abaqus but I struggle to apply the viscous stress. I am looking for a way to apply a non-uniform vector field on the 3D model from a *.csv file. Such a file is linked to this post, there are 6 columns in it. 3 for the application point of the force and 3 others for the force components. Is there any solution to my problem ?

Thanks,

Antoine

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