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- W181815360 abstract "The effects of propeller slipstream on the wing laminar boundary are being investigated. Hot-wire velocity sensor measurements have been performed in flight and in a wind tunnel. It is shown that the boundary layer cycles between a laminar state and a turbulent state at the propeller blade passage rate. The cyclic length of the turbulent state increases with decreasing laminar stability. Analyses of the time varying velocity profiles show the turbulent state to lie in a transition region between fully laminar and fully turbulent. The observed cyclic boundary layer has characteristics similar to relaminarizing flow and laminar flow with external turbulence." @default.
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- W181815360 date "1985-01-01" @default.
- W181815360 modified "2023-09-26" @default.
- W181815360 title "Propeller slipstream/wing boundary layer effects at low Reynolds numbers" @default.
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