[Nek5000-users] Export surface data only

nek5000-users at lists.mcs.anl.gov nek5000-users at lists.mcs.anl.gov
Thu Apr 7 23:30:49 CDT 2016


Hi Paul,
Thanks for that tip. On a follow up question, how would you normally go
about getting the pressure coefficient plot along a section of the airfoil?
For wxample, I would like to get the plot of "Cp versus x" at a particular
section of the airfoil. Do I need to know the node/element numbers to do
this?


Cheers
Rif
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