The use of CFD in the redesign of a model scale rotor for the investigation of stall onset and alleviation for the UKVLN rotor rig

dc.contributor.author Woodgate, M.A.
dc.contributor.author Fitzgibbon, T.A.
dc.contributor.author Barakos, G.N.
dc.date.accessioned 2024-04-17T10:38:32Z
dc.date.available 2024-04-17T10:38:32Z
dc.date.issued 2020
dc.description.abstract An experimental setup has been designed to example in the effect of rotor blade stall flutter. The blade has to be designed so that it does not exceed the maximum permissible load on the rotor rig to be employed for wind tunnel tests, while maximising the blade loading to allow for the blade to be excited. An original set of blades where first tested to examine the possibility of their reuse. On discovery that they required too much power drive them at the required collective computational fluid dynamics (CFD) was used to aid a new design.
dc.identifier.other 1288 erf2020
dc.identifier.uri https://hdl.handle.net/20.500.11881/4166
dc.language.iso en
dc.title The use of CFD in the redesign of a model scale rotor for the investigation of stall onset and alleviation for the UKVLN rotor rig
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