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- W4206449630 abstract "An experimental study was conducted to investigate dynamic ice accretion process on the rotating aero-engine fan blades and evaluate its effects on the aerodynamic performance of the fan rotor. The experiments were performed in an icing research tunnel with a scaled aero-engine spinner-fan model exposed to typical dry rime and wet glaze icing conditions. Under the rime icing condition, while the accreted ice layers were found to conform well with the original shapes of the fan blades in general, the aerodynamic performance of the fan rotor was found to degrade substantially due to the much rougher surfaces of the iced fan blades, causing up to 60% reduction in the pressure increment of the airflow after passing the iced fan rotor after 360 seconds of the rime icing experiment. Much more complicated, needle-like icicles were found to grow rapidly out from the surfaces of the rotating spinner and fan blades under the glaze icing condition, due to the combined effects of the aerodynamic forces and the centrifugal forces associated with the rotation motion. The irregular-shaped, icicle structures accreted on the spinner and fan blades were found to induce massive airflow separations and cause tremendous detrimental effects on the aerodynamic performance of the fan rotor. As a result, the airflow was found to become depressurized, instead of being pressurized, after passing the iced fan rotor. The spinner-fan model was always found to consume more power under the icing condition, Despite of different types of ice structures accreted over the fan blades." @default.
- W4206449630 created "2022-01-26" @default.
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- W4206449630 date "2022-01-03" @default.
- W4206449630 modified "2023-09-23" @default.
- W4206449630 title "An Experimental Study on the Dynamic Ice Accretion Process over the Surfaces of the Rotating Fan Blades of an Aero-Engine Model" @default.
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- W4206449630 doi "https://doi.org/10.2514/6.2022-2435" @default.
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