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validation data for 3D naca00xx section airfoil |
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August 9, 2005, 14:24
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validation data for 3D naca00xx section airfoil
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#1 |
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Guest
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I newly wrote a 3D Euler code and was going to valide the code with NACA 00xx airfoil(3D finite wing).
Does any body have the experimental or computational sectional pressure distribution? |
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August 17, 2005, 10:37
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Re: validation data for 3D naca00xx section airfoi
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#2 |
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Guest
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As a first step one can think of casting 2D flow as 3D. Can consider standard AGARD test cases ( free stream Mach number 0.63 and Angle of attack of 2deg or the other transonic test case). One should carefully implement periodic boundary condition.
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