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Most biological flyers undergo orderly deformation in flight, and thedeformations of wings lead to complex fluid-structure interactions. In thispaper, an aerodynamic-structural coupling method of flapping wing is developedbased on ANSYS to simulate the flapping of flexible wing. Fluent module andTransient Structural module are connected through the System Coupling module tomake a two-way fluid-structure Coupling computational framework. Comparing withthe rigid wing of a cicada, the coupling results of the flexible wing showsthat the flexible deformation can increase the aerodynamic performances offlapping flight.

Dynamic aerodynamic-structural coupling numerical simulation on the flexible wing of a cicada based on ansys