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Update Dynamic_FSI_Python.md
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_tutorials/multiphysics/Unsteady_FSI_Python/Dynamic_FSI_Python.md

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Where $$m$$ is the mass of the airfoil, $$I$$ the inertia around the center of mass, $$S$$ the static moment of inertia at the rotation axis, $$C$$ and $$K$$ the dampings and stiffnesses respectively. $$L$$ and $$M$$ are the lift and pitching up moment.
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Where $$m$$ is the mass of the airfoil, $$I$$ the inertia around the rotation axis, $$S$$ the static moment of inertia at the rotation axis, $$C$$ and $$K$$ the dampings and stiffnesses respectively. $$L$$ and $$M$$ are the lift and pitching up moment.
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These equations are usually adimensionalised to obtain results independent from the free-stream density of the flow.
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Indeed, we can define the following parameters:

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