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Calculating lift over an airfoil

Question asked by Stevie Mixon on Jul 31, 2020

I need to calculate the lift generated if that airfoil was moving through air at sea level  at a velocity of 100 m/s.  Resolve those distributed loads into evenly spaced loads over the edges of the airfoils.  Calculate the maximum deflection of the airfoil and the von Mises stress. 

 

Every time I run the flowsimulation I get errors that say cannot find faces associated with this item.

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