Learning to use ANSYS Fluent as part of my computational engineering course I have previously modelled a 2D wing and been abled to XY plot for the pressure coefficient against x coordinate.
my struggle is when within a 3D case, how do you plot pressure coefficient against at various points across the span line?
the wing is an Onera M6 wing.
where i want to plot 6 separate XY plots of C_p against X/m at each solid line, moving up the dotted span line.
