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Article Dans Une Revue International Journal of Micro Air Vehicles Année : 2019

Rotor performance enhancement through blade surging

Résumé

This short paper introduces a new concept of rotor where the blades undergo a periodic surging motion in the rotor disk plane. It is shown that the unsteady actuation induces aerodynamic phenomenon that can enhance both rotor thrust and efficiency, depending on the amplitude and frequency of actuation. In particular, the increase in aerodynamic performance is found to correlate with the development of a large scale leading edge vortex. Accordingly, the optimal frequency is found to correlate with the formation time of this vortex.
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Origine : Publication financée par une institution

Dates et versions

hal-03041153 , version 1 (04-12-2020)

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Tarek Bensebaa, Thierry Jardin, Sébastien Prothin, Nicolas Doué. Rotor performance enhancement through blade surging. International Journal of Micro Air Vehicles, 2019, 11, pp.1-7. ⟨10.1177/1756829319844275⟩. ⟨hal-03041153⟩
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