Numerical-experimental correlation of rotor flowfield in ground effect

dc.contributor.authorPasquali, C.
dc.contributor.authorSerafini, J.
dc.contributor.authorBernardini, G.
dc.contributor.authorGennaretti, M.
dc.contributor.authorMilluzzo, J.
dc.contributor.authorDavids, S.
dc.date.accessioned2021-03-04T15:52:45Z
dc.date.available2021-03-04T15:52:45Z
dc.date.issued2018
dc.description.abstractThis work presents the comparison between experimental measurements and numerical simulations concerning the flowfield generated by a helicopter rotor operating in ground effect conditions above an inclined plane. Specifically, the capability of a potential-based, three-dimensional, free-wake aerodynamic solver to simulate in-ground-effect problems is assessed in terms of loads and wake inflow field, showing a good agreement with the experimental data.
dc.identifier.other91 - Numerical-Experimental Correlation of Rotor Flowfield in Ground Effect.pdf
dc.identifier.urihttp://hdl.handle.net/20.500.11881/3992
dc.language.isoen
dc.titleNumerical-experimental correlation of rotor flowfield in ground effect

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