The finite element multibody technique is applied to the aeroelastic modeling of tilt-rotors. We analyze the model of a realistic aircraft configuration, and we compare alternative techniques for measuring its aeroelastic stability.
Aeroelastic Simulation of Tilt-Rotors Using Non-Linear Finite Element Multibody Procedures
BOTTASSO, CARLO LUIGI
2003-01-01
Abstract
The finite element multibody technique is applied to the aeroelastic modeling of tilt-rotors. We analyze the model of a realistic aircraft configuration, and we compare alternative techniques for measuring its aeroelastic stability.File in questo prodotto:
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