PANUKL Help - ITLiMS
PANUKL Help - ITLiMS
PANUKL Help - ITLiMS
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Fig. 41 – Selecting result file with aerodynamic characteristics for an airfoil<br />
When *.txt file is loaded: Show Drag polar, Show Lift coefficient, Show Moment coefficient<br />
functions turn active.<br />
Fig. 42 – Example results CL, CD, CM versus Angle of Attack<br />
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