Topometry FEM optimization of the wing structure of the transport aircraft

The article presents the topometry optimization of the critical semi-shell wing structure of the aircraft in the Commuter category of the CS-23 regulation standard (EASA 2012). Modern finite element (FE) optimization methods are used. The main outcome is that the milled integral lower wing panel all...

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Veröffentlicht in:	Aviation (Vilnius, Lithuania) Lithuania), 2017-01, Vol.21 (1), p.29-34
Hauptverfasser:	Katrnak, Tomas, Juracka, Jaroslav
Format:	Artikel
Sprache:	eng
Schlagworte:	Categories Durability FEM Finite element method Mathematical analysis Mathematical models Optimization stress analysis topometry optimization Weight reduction wing structure Wings (aircraft)
Online-Zugang:	Volltext
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