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Journal ArticleDOI

The effect of delaminations on local buckling in wind turbine blades

Philipp Ulrich Haselbach, +2 more
- 01 Jan 2016 - 
- Vol. 85, pp 295-305
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TLDR
In this article, the effect of delaminations on the load carrying capacity of a large wind turbine blade is studied numerically, and it is concluded that delamination induced near-surface buckling modes have to be considered critical due to an onset of local sublaminate buckling below the design load level.
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This article is published in Renewable Energy.The article was published on 2016-01-01. It has received 53 citations till now. The article focuses on the topics: Delamination & Buckling.

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Citations
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Journal ArticleDOI

Damage detection techniques for wind turbine blades: A review

TL;DR: A comprehensive review of state-of-the-art damage detection techniques for WTBs, including most of those updated methods based on strain measurement, acoustic emission, ultrasound, vibration, thermography and machine vision are provided.
Journal ArticleDOI

Linear and nonlinear features and machine learning for wind turbine blade ice detection and diagnosis

TL;DR: This paper presents a novel approach to detect and classify ice thickness based on pattern recognition through guided ultrasonic waves and Machine Learning, and considers four feature extraction methods to validate the results.
Journal ArticleDOI

Delamination analysis in composite laminates by means of Acoustic Emission and bi-linear/tri-linear Cohesive Zone Modeling

TL;DR: In this paper, a combination of acoustic emissions (AE) signal localizations and scattering reduction procedure is implemented to determine the delamination tip position, and a tri-linear CZM can accurately determine both the initiation and propagation of delamination in the existence of fiber bridging.
Journal ArticleDOI

Impact assessment of a wind turbine blade root during an offshore mating process

TL;DR: In this article, a realistic scenario of the mating process and the consequences of such impact loads was investigated, and the results showed severe bending and plastic deformation of the guide pin bolt together with failure of the adjoining composite laminate at the root connection.
Journal ArticleDOI

Experimental investigation on structural collapse of a large composite wind turbine blade under combined bending and torsion

TL;DR: In this paper, the structural collapse of a composite blade under combined bending and torsion in a full-scale static load test was investigated and it was found that longitudinal compressive crushing failure and the following delamination of the spar cap are the root causes of the blade collapse.
References
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Journal ArticleDOI

Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus

TL;DR: In this paper, the authors evaluated the initiation of cracking and delamination growth in a unidirectional glass/epoxy composite under mode I, mode ZZ, and mixed mode I + II static loading.
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Numerical simulation of mixed-mode progressive delamination in composite materials

TL;DR: In this paper, a new decohesion element with the capability of dealing with crack propagation under mixed-mode loading is proposed and demonstrated, which is used at the interface between solid finite elements to model the initiation and non-self-similar growth of delaminations in composite materials.
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Lamina properties, lay-up configurations and loading conditions for a range of fibre-reinforced composite laminates

TL;DR: In this article, the authors present a description of the laminates provided to all participants in an exercise to predict the strength of composite Laminates, including the elastic constants and the stress/strain curves for four unidirectional laminae.
Journal ArticleDOI

On the Flexure of Thin Cylindrical Shells and Other "Thin" Sections

TL;DR: In this article, it is shown that St. Venant's solution of the flexure problem is not supported by ordinary engineering practice, and recent experience in the use of high tensile steels and problems of aircraft structure have emphasised the desirability of a further examination of the Flexure problem.
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