Cp data for Airfoils and Simple Shapes -- CFD Online Discussion Forums

June 11, 2001, 10:58	Cp data for Airfoils and Simple Shapes	#1
Khurram Guest Posts: n/a	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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