Multi-scale least-weight design of a wing-box through a global/local modelling approach
DOI10.1007/S10957-020-01693-YzbMath1468.90097OpenAlexW3037353413MaRDI QIDQ2025711
Marco Montemurro, Francesco Coccia, Daniele Fanteria, Enrico Panettieri
Publication date: 14 May 2021
Published in: Journal of Optimization Theory and Applications (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s10957-020-01693-y
Applications of mathematical programming (90C90) Nonconvex programming, global optimization (90C26) Nonlinear programming (90C30) Sensitivity, stability, parametric optimization (90C31) Finite element methods applied to problems in solid mechanics (74S05) Thin bodies, structures (74K99)
Cites Work
- Variational analysis and aerospace engineering. Mathematical challenges for the aerospace of the future. Based on the presentations at the workshop, Erice, Italy, 2015
- The Automatic Dynamic Penalisation method (ADP) for handling constraints with genetic algorithms
- A general hybrid optimization strategy for curve fitting in the non-uniform rational basis spline framework
- A two-level procedure for the global optimum design of composite modular structures -- application to the design of an aircraft wing
- An efficient zooming method for finite element analysis
- A global-local finite element method suitable for parallel computations
- A refined global‐local finite element analysis method
- Aggressive submodelling of stress concentrations
- A two-level procedure for the global optimum design of composite modular structures -- application to the design of an aircraft wing
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