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Old   April 9, 2008, 13:04
Default Iviscid Flow
John Smith
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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....?
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Old   April 9, 2008, 13:18
Default Re: Iviscid Flow
John Smith
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Sorry I forget to mention that the aerofoil is at an angle 0f attack of 6 degrees
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