Finding Cp- Pressure coefficient -- CFD Online Discussion Forums

November 13, 2017, 19:00	Finding Cp- Pressure coefficient	#1
FluidAerodynamics New Member California Join Date: Nov 2017 Posts: 2 Rep Power: 0	ello, I am trying to find Cp at different spans of a 3d wing airfoil- 0.2, 0.44, 0.8, 0.95. I do not how to find the both x-points of the chord. Please help ASAP. I could do the 0.2 Cp because both the x points at the chord ends were known, But I don't know the same for the different spans. Please let me know asap.!

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