A hybrid multilevel approach for aeroelastic optimization of composite wing-box

DOI10.1007/s00158-009-0429-6zbMath1274.74166OpenAlexW2067560940MaRDI QIDQ381345

Mohammad Hasan, H. S. Yoon

Publication date: 15 November 2013

Published in: Structural and Multidisciplinary Optimization (Search for Journal in Brave)

Full work available at URL: http://urlib.net/sid.inpe.br/mtc-m18@80/2008/12.18.17.43

zbMATH Keywords

structural optimizationcomposite structuresgenetic algorithmmultilevel optimization

Mathematics Subject Classification ID

Quadratic programming (90C20) Plates (74K20) Finite element methods applied to problems in solid mechanics (74S05) General aerodynamics and subsonic flows (76G25) Compliance or weight optimization in solid mechanics (74P05)

Uses Software

• Genocop

Cites Work

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• An SQP method for general nonlinear programs using only equality constrained subproblems
• Lifting surface in subsonic unsteady regime
• Structural optimization by multilevel decomposition
• A superlinearly convergent method of feasible directions.

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