Nonlinear aeroelastic stability analysis of a two-stage axially moving telescopic wing by using fully intrinsic equations
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DOI: 10.1177/09544100221080117
Abstract: During the process of span extension for an aircraft wing equipped with a telescopic morphing mechanism, the wing aspect ratio increases, and hence, the geometrical nonlinearities might become more significant. In this regard, this paper… read more here.
Keywords: intrinsic equations; using fully; telescopic wing; telescopic ... See more keywords