Design and testing of aeroelastically tailored composite wing under fatigue and gust loading including effect of fatigue on aeroelastic performance
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DOI: 10.1016/j.compstruct.2021.114373
Abstract: Abstract The aim of the paper is to experimentally validate a numerical design methodology for optimizing composite wings subject to gust and fatigue loading requirements and to assess the effect of fatigue on the aeroelastic… read more here.
Keywords: fatigue; fatigue aeroelastic; methodology; design ... See more keywords