A Scalable, Parallel Approach for Multi-point, High-fidelity Aerostructural Optimization of Aircraft Configurations
This thesis presents new tools and techniques developed to address the challenging problem of high-fidelity aerostructural optimization with respect to large numbers of design variables. A new mesh-movement scheme is developed that is both computationally efficient and sufficiently robust to accommo...
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| Language: | en_ca |
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2013
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| Online Access: | http://hdl.handle.net/1807/35861 |