validation data for 3D naca00xx section airfoil

August 9, 2005, 14:24

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?

August 17, 2005, 10:37

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.

August 9, 2005, 14:24	validation data for 3D naca00xx section airfoil	#1
Juhee Lee Guest Posts: n/a	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?

August 17, 2005, 10:37	Re: validation data for 3D naca00xx section airfoi	#2
Munikrishna Guest Posts: n/a	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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