Design of rectangular sandwich panels with metal skins based on post-buckling state in compression and shear

Solutions of geometrically non-linear tasks concerning post-buckling behavior of sandwich panels with thin metal skins and lightweight filler loaded by compression and shear flows are shown. Based on obtained solutions methods of aircraft structures sandwich panels design based on post-buckling stat...

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Veröffentlicht in:	IOP conference series. Materials Science and Engineering 2019-11, Vol.684 (1), p.12020
1. Verfasser:	Mitrofanov, O V
Format:	Artikel
Sprache:	eng
Schlagworte:	Aircraft design Aircraft structures Postbuckling Sandwich panels Shear flow
Online-Zugang:	Volltext
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Beschreibung
Zusammenfassung:	Solutions of geometrically non-linear tasks concerning post-buckling behavior of sandwich panels with thin metal skins and lightweight filler loaded by compression and shear flows are shown. Based on obtained solutions methods of aircraft structures sandwich panels design based on post-buckling state with acceptable global buckling in case of ultimate loading are suggested.
ISSN:	1757-8981 1757-899X
DOI:	10.1088/1757-899X/684/1/012020