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- W4206176690 abstract "Determining trim flight conditions for a rotorcraft requires a proper understanding of the impact of aeroelastic deformation of its rotor blades. Such simulations are often neglected during preliminary design due to the associated high computational cost. In this work it is demonstrated that the uncoupled static aeroelastic analysis method can be used to efficiently and inexpensively compute the aeroelastic deformation of a rotor blade throughout the entire rotor disk. Results show that utilizing the uncoupled static aeroelastic analysis method can enable rapid determination of changes in the coefficient of lift due to aeroelastic deformation." @default.
- W4206176690 created "2022-01-26" @default.
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- W4206176690 date "2022-01-03" @default.
- W4206176690 modified "2023-10-02" @default.
- W4206176690 title "Analysis of Rotor Blade Aeroelastic Deformation Utilizing the Uncoupled Static Aeroelastic Analysis Method" @default.
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- W4206176690 doi "https://doi.org/10.2514/6.2022-2555" @default.
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