I can't use pressure results from fluent to perform one-way fsi with wing model in mechanical in static structural.

I need to apply the pressure on my model wing, but i cannot link the geometry from fluent to static structural. I need to use the pressure result to apply to the model wing for structural analysis.

How do i do this?  Is this possible?

Thanks for your help, I am running out of time on my project and have been stuck at this point for many weeks now trying to get achieve this setup.