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Iviscid Flow

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April 9, 2008, 13:04	Iviscid Flow	#1
John Smith Guest Posts: n/a	When solving for inviscid flow around a NACA44012 aerofoil, I still get drag values is this due to Artificial Viscosity or down to pressure drag....?

April 9, 2008, 13:18	Re: Iviscid Flow	#2
John Smith Guest Posts: n/a	Sorry I forget to mention that the aerofoil is at an angle 0f attack of 6 degrees

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