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Development of an optimization framework for landing gear design
Landing Gear Design Integration for the TU Delft Initiator
Wing aerostructural optimization using the Individual Discipline Feasible architecture
Supporting MDO through dynamic workflow (re)generation
Multidisciplinary Design Optimization in the Conceptual Design Phase: Creating a Conceptual Design of the Blended Wing-Body with the BLISS Optimization Strategy
Wing Shape Multidisciplinary Design Optimization
SAS: an advisory framework to support surrogate model based MDAO
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