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Cp data for Airfoils and Simple Shapes

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Old   June 11, 2001, 10:58
Default Cp data for Airfoils and Simple Shapes
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i need Cp data for 4-5 Digit Naca airfoils. I some of you have done validation with any CFD code, i would like to have that data. Moreover i also require Cp distribution over simple shapes like sphere(circle-2d), cones etc. please mention reference conditions (mach, angle of attack and reynold no) alongwith the boundry conditions. if some one is interested in joint research in this area i would love to do it. thanks
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