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March 19, 2012, 06:25 |
Extracting data from 3D domain
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#1 |
New Member
Rachit Prasad
Join Date: Jun 2011
Location: Blacksburg, Virginia
Posts: 29
Rep Power: 14 |
Hi everyone,
I have been doing 3D simulations over a NACA 0012 wing using StarCCM+. I wanted to plot the pressure coefficient over the airfoil at the wing base. I have done that for 2D simulations using the XY plot. However, how could I accomplish that for 3D simulations? What I thought of was to make a derived part plane section at the wing base, but then how do I get the value of pressure coefficients on the airfoil from it? Any ideas? Thanks in advance! Regards, Rachit |
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