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- W4311960392 abstract "This study relates the structural deformation and the unsteady aerodynamics involved for lift production in bioinspired nanocomposite flapping wings. The sectional chord deformation effects on theoretically supported aerodynamic lift are addressed. Digital image correlation setup and L-shape mechanism are developed and synchronized for wing deformation and aerodynamic forces measurement respectively. DIC system with estimated resolution of 0.159 mm/pixel and L-shape mechanism with net uncertainty of ±0.72% verify the measurement accuracy for low Reynolds number flapping wing experiments and alike miniature aero-structures. The flapping wing shape is investigated at 25%, 50% and 75% wing-span to study the effect of sectional chord deformation on lift components obtained from Theodorsen theory. Circulatory lift is dominant at mid-downstroke while Non-circulatory lift is dominant at the beginning of flapping cycle due to inertial effects." @default.
- W4311960392 created "2023-01-03" @default.
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- W4311960392 date "2022-12-09" @default.
- W4311960392 modified "2023-10-18" @default.
- W4311960392 title "Aerostructural evaluation of bioinspired chordwise flexible flapping wing" @default.
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- W4311960392 doi "https://doi.org/10.1080/15376494.2022.2153187" @default.
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