Aircraft Design 2 – Stability calculation with AVL - ITLiMS
Aircraft Design 2 – Stability calculation with AVL - ITLiMS
Aircraft Design 2 – Stability calculation with AVL - ITLiMS
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The Faculty of Power and Aeronautical Engineering of Warsw Uniwersity of Technology <strong>–</strong> <strong>Aircraft</strong> <strong>Design</strong> Department<br />
Requirements:<br />
Aerodynamic analysis (OPER)<br />
o Plot of geometry <strong>with</strong> pressure loads<br />
o List of aerodynamic derivatives<br />
o Neutral point in percents of MAC<br />
Jacek Mieloszyk <strong>–</strong> Project Guide: Longitudinal static stability and control 2/2
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