Experimental characterisation of flutter and divergence of 2D wing section with stabilised response
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DOI: 10.1016/j.ast.2018.05.014
Abstract: Abstract The first experimental application of the Parametric Flutter Margin method for identification of aeroelastic instabilities is presented. The experiment was performed in two steps using a two degree-of-freedom wing segment mounted in the wind… read more here.
Keywords: methodology; response; parametric flutter; flutter divergence ... See more keywords