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- W2317548231 abstract "Continuous requirements for more efficient, greener aircrafts drive the design and analysis of novel propulsion configurations. A promising concept is expected to be the distribution of propulsion systems along the span of the wing. One of the benefits from distributed propulsion is the ingestion of the boundary layer that develops on the suction surface, with a direct effect on propulsive efficiency and fuel saving. However, the reenergization of low momentum boundary layer flow, introduces an inherent complexity to the design of the fan, as the flow that hits the fan face is characterized by highly distorted velocity profiles, due to low inlet velocity region at the lower part of the inlet circumference . As a result, each fan blade operates under varying inlet conditions during every revolution, something that has an impact on both aerodynamic performance but also mechanical integrity of the fan. The present paper focuses on the mechanical dynamic response of a fan blade operating under inlet distortion that could result from a boundary layer ingesting configuration." @default.
- W2317548231 created "2016-06-24" @default.
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- W2317548231 date "2012-07-30" @default.
- W2317548231 modified "2023-09-25" @default.
- W2317548231 title "Dynamic Response and High Cycle Fatigue Analysis of Fan Blades under Inlet Distortion" @default.
- W2317548231 cites W2099724657 @default.
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- W2317548231 doi "https://doi.org/10.2514/6.2012-3770" @default.
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