aerofoil lift and drag curves (with automatic excecution)
 

is it true that when doing the automatic excecution of different files, once iteration has been done and saved etc. that the lift, drag and momentum curves can not be retreived when re-reading the file case and data. Is this data inaccurate due to computational reasons or is it important and accurate? do i need these graphs and if yes can i retreave them after automatic excecution? if so how?