Maximum stiffness and minimum weight optimization of laminated composite beams using continuous fiber angles

DOI10.1007/s00158-010-0592-9zbMath1274.74260OpenAlexW2061907835WikidataQ56050715 ScholiaQ56050715MaRDI QIDQ381589

Mathias Stolpe, José Pedro Blasques

Publication date: 15 November 2013

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

Full work available at URL: https://doi.org/10.1007/s00158-010-0592-9

zbMATH Keywords

beamslaminated compositescompliance and weight optimization

Mathematics Subject Classification ID

Optimization of other properties in solid mechanics (74P10)

Related Items (1)

Concurrent topology optimization of structures and orientation of anisotropic materials

Uses Software

• SNOPT

Cites Work

• A Newton method for solving continuous multiple material minimum compliance problems
• Parametrization in laminate design for optimal compliance
• Discrete material optimization of general composite shell structures
• Optimization of laminate stacking sequence for buckling load maximization by genetic algorithm
• Sensitivity analysis and design optimization of three-dimensional non-linear aeroelastic systems by the adjoint method
• SNOPT: An SQP Algorithm for Large-Scale Constrained Optimization
• Assessment of beam modeling methods for rotor blade applications.

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