OPTIMIZATION OF COMPOSITE AIRCRAFT STRUCTURES IN CONSIDERATION OF POSTBUCKLING BEHAVIOR

DOI10.1142/S0219455410003804zbMath1416.74078OpenAlexW2124177466MaRDI QIDQ3002043

Fernaß Daoud, Mircea Calomfirescu

Publication date: 19 May 2011

Published in: International Journal of Structural Stability and Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1142/s0219455410003804

zbMATH Keywords

weight minimizationgradient-based optimizationskin buckling

Mathematics Subject Classification ID

Composite and mixture properties (74E30) Bifurcation and buckling (74G60) Compliance or weight optimization in solid mechanics (74P05)

Uses Software

• LAGRANGE

Cites Work

• On the convergence of a sequential quadratic programming method with an augmented lagrangian line search function

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