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Published in 2019 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2019.105321
Abstract: Abstract This article describes the aerodynamic design and assessment of a UCAV wing developed under the NATO-STO AVT-251 Multi-disciplinary Design Task Group. The wing design rationale and process is described, as well as how the…
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Keywords:
design assessment;
comparisons muldicon;
aerodynamic design;
muldicon ucav ... See more keywords