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This article presents a comparative study of three numerical algorithms for computation of the flow-field of a rotor in hover and the net static thrust that is produced. The flow-field is induced by a series of vortex rings. modelling the near wake of the hovering rotor and a single semi-infinite vortex cylinder. accounting for the velocity deficit in the far wake. https://danddcollectiblers.shop/product-category/cooker/
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