Analysis of the deformation energy of straight composite z-frames subjected to critical buckling loads

In this paper the correlation of deformation energy and critical buckling loads is examined. An advanced analysis technique is derived for the investigation of z-section frames typically applied in composite aircraft fuselage. This technique is verified through closed form solutions of z-section col...

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Veröffentlicht in:	Finite elements in analysis and design 2015-06, Vol.98, p.50-60
Hauptverfasser:	Weiß, L., Köke, H., Rohwer, K., Hühne, C., Wiedemann, M.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerospace Aircraft Aircraft components Buckling Crashes Deformation Exact solutions Frames Fuselages Mathematical analysis Structural analysis Z-section column
Online-Zugang:	Volltext
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