Rigid Body 2D analysis
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Hi Guys, I want to simulate the behaviour of rear wing support with 2D Mechanical analysis (Image).
So my idea is to set the airfoil as rigid body with a force on the upper side to evaluate the stress only on support . But, when I do this, the software not define the geometry and also the analysis.
What is the right way to do this simulation? What is wrong in my idea?
the contact region is defined and the material too.
I know how to set fixed supports and forces but the problem I think is on the definition
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