A recent consideration in aircraft design is the use of folding wingtips, with the aim of enabling higher-aspect-ratio wings with less induced drag but also meeting airport gate limitations. A formulation is introduced to account for finite rotations of rigid folding wingtips attached through hinges on a flexible airframe structure including also aerodynamic follower forces for the folding wingtip components. This study investigates the effects of geometric nonlinearities on the quasi-steady aeroelastic response of floating wingtips. It is found that the wingtip response can vary significantly when geometric nonlinearities are accounted for; however, a small impact was observed on the main airframe structure.
Quasi-steady aeroelastic analysis of the semi-aeroelastic hinge including geometric nonlinearities / Conti, C.; Saltari, F.; Mastroddi, F.; Wilson, T.; Castrichini, A.. - In: JOURNAL OF AIRCRAFT. - ISSN 0021-8669. - 58:5(2021), pp. 1168-1178. [10.2514/1.C036115]
Quasi-steady aeroelastic analysis of the semi-aeroelastic hinge including geometric nonlinearities
Conti C.
;Saltari F.;Mastroddi F.;
2021
Abstract
A recent consideration in aircraft design is the use of folding wingtips, with the aim of enabling higher-aspect-ratio wings with less induced drag but also meeting airport gate limitations. A formulation is introduced to account for finite rotations of rigid folding wingtips attached through hinges on a flexible airframe structure including also aerodynamic follower forces for the folding wingtip components. This study investigates the effects of geometric nonlinearities on the quasi-steady aeroelastic response of floating wingtips. It is found that the wingtip response can vary significantly when geometric nonlinearities are accounted for; however, a small impact was observed on the main airframe structure.File | Dimensione | Formato | |
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Note: https://doi.org/10.2514/1.C036115
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