Electroactive morphing effects on the aerodynamic performance through wobulation around an A320 wing with vibrating trailing edge at high Reynolds number

Rouaix, C.; Jiménez-Navarro, C.; Carvalho, M.; Raibaudo, C.; Abou-Khalil, J.; Marouf, A.; Hoarau, Y.; Harran, G.; Hunt, J.C.R.; Hangan, H.; Rouchon, J.F.; Braza, M.

doi:10.1016/j.jfluidstructs.2023.104016

Journal of Fluids and Structures

2023

DOI: 10.1016/j.jfluidstructs.2023.104016

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Electroactive morphing effects on the aerodynamic performance through wobulation around an A320 wing with vibrating trailing edge at high Reynolds number

C. Rouaix,

C. Jiménez-Navarro,

M. Carvalho

et al.

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2024

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Cited by 3 publications

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Experimental closed-loop flow separation control: Data- and phenomenological-driven approaches

Arnoult,

Acher,

Nowinski

et al. 2024

European Journal of Control

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Experimental closed-loop flow separation control: Data- and phenomenological-driven approaches

Arnoult,

Acher,

Nowinski

et al. 2024

European Journal of Control

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Editorial for the “Special Issue in Honor of Emmanuel de Langre”

Modarres-Sadeghi

2024

Journal of Fluids and Structures

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Size-Dependent Finite Element Analysis of Functionally Graded Flexoelectric Shell Structures Based on Consistent Couple Stress Theory

Deng,

Shang

2024

Aerospace

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The functionally graded (FG) flexoelectric material is a potential material to determine the structural morphing of aircrafts. This work proposes the penalty 20-node element based on the consistent couple stress theory for analyzing the FG flexoelectric plate and shell structures with complex geometric shapes and loading conditions. Several numerical examples are examined and prove that the new element can predict the size-dependent behaviors of FG flexoelectric plate and shell structures effectively, showing good convergence and robustness. Moreover, the numerical results reveal that FG flexoelectric material exhibits better bending performance and higher flexoelectric effect compared to homogeneous materials. Moreover, the increase in the material length scale parameter leads to a gradual increase in the natural frequencies of the out-of-plane modes of FG flexoelectric plate/shell, while the natural frequencies of the in-plane modes change minimally, resulting in the occurrence of mode-switching phenomena.

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Electroactive morphing effects on the aerodynamic performance through wobulation around an A320 wing with vibrating trailing edge at high Reynolds number

Cited by 3 publications

References 65 publications

Experimental closed-loop flow separation control: Data- and phenomenological-driven approaches

Experimental closed-loop flow separation control: Data- and phenomenological-driven approaches

Editorial for the “Special Issue in Honor of Emmanuel de Langre”

Size-Dependent Finite Element Analysis of Functionally Graded Flexoelectric Shell Structures Based on Consistent Couple Stress Theory

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