Project report from basic science initiative to use Hierarchical Asynchronous Parallel Evolutionary Algorithms for MDO of a UAV system using high fidelity analysis tools. Two production UAV wings were examined for aerodynamic and structural properties. Optimization was performed over 48 design variables.
Multi-Objective and Multidisciplinary Design Optimisation (MDO) of UAV Systems using Hierarchical Asynchronous Parallel Evolutionary Algorithms
2007
100 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aircraft , Computer Software , Fluid Mechanics , Wings , Software tools , Algorithms , Optimization , Finite element analysis , Australia , Computational fluid dynamics , Drones , Mdo(Multidisciplinary design optimisation) , Foreign reports , Hierarchical asynchronous parallel evolutionary algorithms , Design variables , Uav(Unmanned aerial vehicles)
British Library Conference Proceedings | 2007
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