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In the Boundary Conditions window, select Inlet. Check to make sure that the Type has correctly defaulted to Velocity-Inlet and press Edit.... In the Momentum Tab, we will specify the velocity of the incoming air.

flow=35 (ft^3)/minute=1008(in^3)/s
u=(1008 (in^3)/s)/((4.72/2 in)^2 π)=57.609in/sImage Added