Nonlinear Static Aeroelasticity of High-Aspect-Ratio-Wing Aircraft by Finite Element and Multibody Methods
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DOI: 10.2514/1.c033825
Abstract: Two procedures for the nonlinear static aeroelastic analysis of flexible high-aspect-ratio wing aircraft subject to geometric nonlinearities are developed. The two approaches are based on the nonlinear finite element method and on multibody dynamics, and… read more here.
Keywords: aircraft; wing aircraft; aspect ratio; ratio wing ... See more keywords