One of the key-elements for high performance aircraft design is to design a high lift system within the given spatial constraints without having to increase the wing area to meet landing speed requirements and therefore to have a lower wing area, that imply less wing weight and less drag. This work address activities performed within the Clean-Aviation UP-Wing project to improve high lift aerodynamics of high aspect ratio wing.
High-Lift Challenges of High-Performance Wings / Mingione, Giuseppe; Wild, Jochen; Bier, Niko; Minervino, Mauro; Luigi Vitagliano, Pier; Marino, Luca; Sodja, Jurij; Trautmann, Tobias; Vellekoop &, Michael; Galasso, Bernardino. - 18:(2026), pp. 59-80. [10.1007/978-3-032-17696-7_5]
High-Lift Challenges of High-Performance Wings
Mauro MinervinoInvestigation
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2026
Abstract
One of the key-elements for high performance aircraft design is to design a high lift system within the given spatial constraints without having to increase the wing area to meet landing speed requirements and therefore to have a lower wing area, that imply less wing weight and less drag. This work address activities performed within the Clean-Aviation UP-Wing project to improve high lift aerodynamics of high aspect ratio wing.| File | Dimensione | Formato | |
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978-3-032-17696-7_Springer-Ch5.pdf
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