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- W584597535 abstract "The trailing vortices from a lifting line propeller model are aligned with the flow in the wake. Both bound and trailing vortices are discretized. The calculated location of the trailing vortices is compared with experiments and the agreement is good. The effect of wake alignment on the induced velocities and on the loading distribution of the propeller is investigated. This effect is compared with the effect of linearization of the bound vortices on a mean helical plane. For light to moderately loaded propellers the effect of wake alignment on thrust is found to be limited (approx. 4%). On skewed propellers the linearization of the bound vortices becomes important." @default.
- W584597535 created "2016-06-24" @default.
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- W584597535 date "1995-01-01" @default.
- W584597535 modified "2023-09-26" @default.
- W584597535 title "THE INFLUENCE OF THE WAKE MODEL ON INDUCED VELOCITIES IN THE PROPELLER PLANE" @default.
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