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Variable Velocity Inlet magnitude and direction

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March 24, 2014, 07:24	Variable Velocity Inlet magnitude and direction	#1
Brendan New Member Join Date: Jul 2013 Posts: 6 Rep Power: 13	Hi everyone, My name is Brendan and I am faced with a small issue when it comes to the velocity inlet for an airfoil simulation. My goal is to have a stationary airfoil and mesh, from this I can apply the inlet and outlet boundary conditions. To determine the optimum angle of attack for that given inlet velocity I want to vary the "x" and "y" components, i.e. sin Y and cos x. Is there any way to complete this so I can plot graphs to prove the findings???? It's out of self interest I am doing this so an help is greatly appreciated. B.

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airfoil, boundary condition, fluent, variable velocity angle, velocity

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