Efficient nonlinear aeroelastic analysis of a morphing wing via parameterized fictitious mode method
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DOI: 10.1007/s11071-021-06577-y
Abstract: The folding wing, as a possible concept for designing morphing aircraft, has gained special attention. However, such a wing may encounter complex nonlinear aeroelastic effects with bilinear-hinge stiffnesses during the in-flight morphing process. This paper… read more here.
Keywords: parameterized fictitious; folding wing; methodology; nonlinear aeroelastic ... See more keywords