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- W2013304037 abstract "This paper reviews aeroelastic analysis methods for propulsion elements (advanced propellers, compressors and turbines) being developed and used at NASA Lewis Research Center. These aeroelastic models include both structural and aerodynamic components. The structural models include the typical section model, the beam model with and without disk flexibility, and the finite element blade model with plate bending elements. The aerodynamic models are based on the solution of equations ranging from the two-dimensional linear potential equation for a cascade to the three-dimensional Euler equations for multi-blade configurations. Typical results are presented for each aeroelastic model. Suggestions for further research are indicated. All the available aeroelastic models and analysis methods are being incorporated into a unified computer program named APPLE (Aeroelasticity Program for Propulsion at LEwis)." @default.
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- W2013304037 date "1992-08-17" @default.
- W2013304037 modified "2023-10-16" @default.
- W2013304037 title "APPLE - An aeroelastic analysis system for turbomachines and propfans" @default.
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- W2013304037 doi "https://doi.org/10.2514/6.1992-4712" @default.
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