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Hybrid OVERFLOW-vortex method solution of 4-bladed rotor (top view)

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Published on Jun 29, 2010

95 Frames from a simulation of a 4-bladed, twisted, rotor in forward flight with advance ratio of 0.23. The data is from a simulation done using a hybrid OVERFLOW-vortex particle method run on a GPU cluster. Illustrated here is an x-ray of the circulation field from the top. Total blade rotation is 970 degrees. See http://markjstock.org/research/ for more details.

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