[OpenFOAM] Output of pressure data -- CFD Online Discussion Forums

February 29, 2020, 08:26	Output of pressure data	#1
Kfpersie New Member jack pory Join Date: Feb 2020 Posts: 1 Rep Power: 0	Hello, this is lantern of OpenFOAM beginner. After performing a steady analysis with the NACA airfoil and outputting the calculated data as a vtk file, the vtk file was read with paraview and the calculated data for the wing part was output. However, only the pressure data on the lower surface of the wing was included in the calculation data, and the data on the pressure on the upper surface of the wing were not output. Anyone know how to output well?

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