Postbuckling of imperfect rectangular composite plates under inplane shear closed-form approximate solutions

DOI10.1007/S00419-010-0491-YzbMath1271.74096OpenAlexW2031787977MaRDI QIDQ364757

Henrike Erdmann, Kai-Uwe Schröder, Christian Mittelstedt

Publication date: 3 September 2013

Published in: Archive of Applied Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s00419-010-0491-y

zbMATH Keywords

stabilitycompositesbucklingpostbucklingshearlaminates

Mathematics Subject Classification ID

Plates (74K20) Composite and mixture properties (74E30) Bifurcation and buckling (74G60) Explicit solutions of equilibrium problems in solid mechanics (74G05)

Cites Work

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• Large amplitude vibration of orthotropic elliptical plates
• Postbuckling response of laminated plates under uniaxial compression
• Post-buckling behaviour of graphite/epoxy stiffened panels with initial imperfections subjected to eccentric biaxial compression loading
• The shear buckling behaviour of thin composite plates with particular reference to the effects of bend-twist coupling
• Analytical effective width equations for limit state design of thin plates under non-homogeneous in-plane loading
• Postbuckling of long unsymmetrically laminated composite plates under axial compression
• POSTBUCKLING OF COMPRESSIVELY LOADED IMPERFECT COMPOSITE PLATES: CLOSED-FORM APPROXIMATE SOLUTIONS
• Thermal buckling of composite laminated plates
• A multi-term semi-energy finite strip method for post-buckling analysis of composite plates

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