how to create surface pressure data file
 

Hi,

I want to plot the pressure distribution of different airfoil configurations on top of one another. So I was wondering if i could somehow output the pressure coefficient at each node along the airfoil into a data file once my case has converged? And if so how would i be able to do this. I know this sound like something easy but havent been able to figure out how to do this yet and have been continually going through the help manuals with no luck.

Thanks