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Inviscid flow around an airfoil NACA0012 using Ansys fluentpart1Geometry
>> YOUR LINK HERE: ___ http://youtube.com/watch?v=jh2yyw2eVH8
In this video we created the Geometry of a flow field with an airfoil NACA0012 with an angle of attack equal to zero through coordinates points that you can find them for several airfoils in the web site airfoiltools.com but you should take them and put them in a text file with the same way I showed in the video. • Thank you • #Ansys #fluent #NACA
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