Efficient Tools for the Simulation of Flapping Wing Flows

The development of novel strategies for lift and propulsion using flapping wings requires the use of computational tools that are at once e!cien t and capable of handling complex deforming boundary motion. In this work we present the use of a viscous vortex particle method for the simulation of the flow produced by a two-dimensional rigid wing in pitching and plunging motion of moderate Reynolds number. By its Lagrangian nature, this method is able to automatically adapt to important flow structures. E! ciency is ensured by using vorticity-bearing computational elements that are distributed only to the extent that vorticity itself is spread through its convection and di"u sion; no e" ort is needed for irrotational regions of flow. Moreover, the correct behavior of the velocity at infinity is automatically satisfied, obviating the need for an artificial boundary treatment. Results of the dynamically shed vorticity and the forces exerted are presented for a single stroke of a flapping elliptical wing.

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