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This paper exposes methodologies and results obtained in a morphing wing application that was developed starting from a full-scaled portion of a real aircraft wing. The experimental model used a full scaled portion of a real aircraft wing, which was
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::84e0636d3508359ba408aa19c98a7970
https://doi.org/10.2514/6.2021-1836
https://doi.org/10.2514/6.2021-1836
