Model-Based and Signal-Based Inverse Methods 2022
DOI: 10.4322/978-65-86503-71-5.c05
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Application of Machine Learning and Multi-Disciplinary/Multi-Objective Optimization Techniques for Conceptual Aircraft Design

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“…By a slight reduction of the wing aspect ratio of the Design ID 303CE (Table 22), keeping the remained parameters but the root airfoil section of the wing unchanged, a baseline airplane was created for this last optimization task (Table 24). Mattos et al [69] applied a flutter speed constraint to an MDO framework for airliner conceptual design. As optimization results, a noticeable reduction of wing aspect ratio was observed when compared with an optimization where no flutter speed constraint was applied.…”
Section: Robust Optimization Of a Chosen Individual Of A Previous Opt...mentioning
confidence: 99%
“…By a slight reduction of the wing aspect ratio of the Design ID 303CE (Table 22), keeping the remained parameters but the root airfoil section of the wing unchanged, a baseline airplane was created for this last optimization task (Table 24). Mattos et al [69] applied a flutter speed constraint to an MDO framework for airliner conceptual design. As optimization results, a noticeable reduction of wing aspect ratio was observed when compared with an optimization where no flutter speed constraint was applied.…”
Section: Robust Optimization Of a Chosen Individual Of A Previous Opt...mentioning
confidence: 99%