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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2017
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Article
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Fig 13
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Review Article
Wind Turbine Aeroelastic Modeling: Basics and Cutting Edge Trends
Figure 13
Fatigue damage equivalent loads D L at the blade root flapwise bending moment. The DEL refers to a 25-year lifetime and 10 million equivalent cycles [
97
].