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- W2034006101 abstract "A nonlinear aeroelastic analysis is developed to analyze the aeroelastic characteristics of flexible high-aspect-ratio wings at transonic speeds. This is achieved by directly coupling a three-dimensional geometric nonlinear methodology, based on a 12 degree-of-freedom beam finite element, with an Euler/Navier-Stokes computational fluid dynamics analysis. Static aeroelastic results are presented for an unswept and swept high-aspect-ratio wing. Unswept wing results show a reversal in twist due to the nonlinear torsion-bending coupling effects. Specifically, the torsional moments due to drag become large enough to cause the wing twist rotations to washin the wing tips, whereas the linear results show a washout twist rotation. The nonlinear twist results are attributed to the large bending displacements coupled with the large drag experienced by this flexible high-aspect-ratio wing at the transonic flow conditions. Swept wing results show that nonlinear torsion-bending effects tend to reduce the amount of washout as compared to a linear structural aeroelastic analysis, making the wing more prone to tip stall." @default.
- W2034006101 created "2016-06-24" @default.
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- W2034006101 date "2005-07-01" @default.
- W2034006101 modified "2023-10-05" @default.
- W2034006101 title "Numerical Investigation of Nonlinear Aeroelastic Effects on Flexible High-Aspect-Ratio Wings" @default.
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- W2034006101 doi "https://doi.org/10.2514/1.6544" @default.
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