Multi-objective Multi-disciplinary Aircraft Wing Optimization
This is the result of an multi-objective multi-disciplinary design optimization of an aircraft wing structure where 3 conflicting objectives were optimized. The result shows the pareto optimality: Improving on one objective requires to sacrifice on the other. This plot helps us understand the trade-offs. Each point is a discrete design which has been automatically analyzed using NASTRAN for FEM and AeolusASP for Aero.
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