Structure Optimization of Large Composite Wing Box with Parallel Genetic Algorithm
Author:
Affiliation:
1. Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031493
Reference8 articles.
1. Two-level composite wing structural optimization using response surfaces
2. Combining a finite element programme and a genetic algorithm to optimize composite structures with variable thickness
3. General Panel Sizing Computer Code and Its Application to Composite Structural Panels
4. Initial sizing optimisation of anisotropic composite panels with T-shaped stiffeners
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