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- W2904904591 abstract "A time-marching aeroelastic method developed for the study of propeller flutter is presentedand validated. Propeller flutter can take many forms with stall, whirl and classical flutterbeing the primary responses. These types of flutter require accurate capture of the non-linearaerodynamics associated with propeller blades. Stall flutter in particular, due to the highlydetached nature of the flow, needs detailed unsteady flow modelling. With the development of modern propeller designs potentially adjusting the flutter boundary and the development of faster computing power, CFD is required to ensure accurate capture of aerodynamics. Thispaper focuses on the validation of the aeroelastic method using the Commander propellerblade." @default.
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- W2904904591 date "2019-01-06" @default.
- W2904904591 modified "2023-09-25" @default.
- W2904904591 title "A Time-Marching Aeroelastic Method Applied to Propeller Flutter" @default.
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- W2904904591 doi "https://doi.org/10.2514/6.2019-1102" @default.
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