2023
DOI: 10.1016/j.compstruct.2023.116680
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Structural transverse cracking mechanisms of trailing edge regions in composite wind turbine blades

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Cited by 8 publications
(1 citation statement)
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“…They have also been considered to calculate peel stresses in a trailing edge adhesive joint [6]. Buckling as another geometrically nonlinear effect was found to be a possible driver for trailing edge damages [7]. However, to the best knowledge of the authors, there is no publication available on the effect of IPCD on the aerodynamic or aeroelastic behavior of the blade.…”
Section: Introductionmentioning
confidence: 99%
“…They have also been considered to calculate peel stresses in a trailing edge adhesive joint [6]. Buckling as another geometrically nonlinear effect was found to be a possible driver for trailing edge damages [7]. However, to the best knowledge of the authors, there is no publication available on the effect of IPCD on the aerodynamic or aeroelastic behavior of the blade.…”
Section: Introductionmentioning
confidence: 99%