2015Acta Scientiarum Naturalium Universitatis SunyatseniRequires access

Adjoint-based optimization of flapping plates hinged with a trailing-edge flap

Мин, Xu, Mingjun, Wei Wei, Chengyu, Li, Haibo, Dong

Open publisher page 6 citations

Abstract

It is important to understand the impact of wing-morphing on aerodynamic performance in the study of flapping-wing flight of birds and insects.We use a flapping plate hinged with a trailing-edge flap as a simplified model for flexible/morphing wings in hovering.The trailing-edge flapping motion is optimized by an adjoint-based approach.The optimized configuration suggests that the trailing-edge flap can substantially enhance the overall lift.Further analysis indicates that the lift enhancement by the trailingedge flapping is from the change of circulation in two ways:the local circulation change by the rotational motion of the flap,and the modification of vortex shedding process by the relative location between the trailing-edge flap and leading-edge main plate.

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What this paper is about

It is important to understand the impact of wing-morphing on aerodynamic performance in the study of flapping-wing flight of birds and insects.We use a flapping plate hinged with a trailing-edge flap as a simplified model for flexible/morphing wings in hovering.The trailing-edge flapping motion is optimized by an adjoint-based approach.The optimized configuration suggests that the trailing-edge flap can substantially enhance the overall lift.Further analysis indicates that the lift enhancement by the trailingedge flapping is from the change of circulation in two ways:the local circulation change by the rotational motion of the flap,and the modification of vortex shedding process by the relative location between the trailing-edge flap and leading-edge main plate.

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Available abstract

It is important to understand the impact of wing-morphing on aerodynamic performance in the study of flapping-wing flight of birds and insects.We use a flapping plate hinged with a trailing-edge flap as a simplified model for flexible/morphing wings in hovering.The trailing-edge flapping motion is optimized by an adjoint-based approach.The optimized configuration suggests that the trailing-edge flap can substantially enhance the overall lift.Further analysis indicates that the lift enhancement by the trailingedge flapping is from the change of circulation in two ways:the local circulation change by the rotational motion of the flap,and the modification of vortex shedding process by the relative location between the trailing-edge flap and leading-edge main plate.

Key concepts: Flapping, Trailing edge, Morphing, Wing, Lift (data mining), Aerodynamics, Leading edge, Aerospace engineering

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