PANUKL Help - ITLiMS
PANUKL Help - ITLiMS
PANUKL Help - ITLiMS
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File [name.CZY]<br />
Aerodynamic coefficients distribution over the wing – results, (Y, Cz, Cm, Cxi, Si, Ci):<br />
Fig. 11 – Example results – Lift coefficient distribution vs. wing span (results from *.CZY file)<br />
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