Abstract
Wind turbine design standards recommend the use of statistical modeling coupled with extrapolation of the short-term load data to long-term periods for fatigue reliability assessment. However, statistical error and computational expense can limit the accuracy of such approaches. In the case of wind turbine blades, the errors are more significant because of the high material fatigue exponent that makes the damage estimations more sensitive to variations. In addition, due to different excitation sources, the flapwise load range histogram is not uni-modal, and thus its statistical modeling is complex. In the present work, we provide three methods for statistical modeling of the flapwise bending moment ranges including a novel approach based on frequency-based separation of the modes. The first two methods are simplified approaches for modeling the most crucial load ranges using unimodal distributions and the third method involves multimodal distribution fitting. The research is based on 3600 10-minute aeroelastic simulations of DTU 10MW case study wind turbine from which a benchmark damage equivalent load (DEL) is calculated. The DEL calculated by each of the three proposed methods is compared to this reference. The results show that the conventional approach based on using 6 seeds can lead to under-conservative results with errors up to 5%. On the other hand, the simplified unimodal approaches provided in this work can provide conservative estimations of the fatigue damage with mean values 5% and 12% higher than the benchmark. However, the variability of the DEL estimates is higher when using unimodal extrapolation of the load ranges, and the data can be conservative by 17.5%. The proposed unimodal fits suggested for modeling and extrapolation of the blade’s load ranges provide less errors relatively and most importantly conservative DEL estimations while maintaining computational efficiency.
Original language | English |
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Publication date | 2023 |
Number of pages | 17 |
Publication status | Published - 2023 |
Event | 2023 AIAA SciTech Forum - National Harbor, United States Duration: 23 Jan 2023 → 27 Jan 2023 |
Conference
Conference | 2023 AIAA SciTech Forum |
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Country/Territory | United States |
City | National Harbor |
Period | 23/01/2023 → 27/01/2023 |
Keywords
- Rainflow matrix
- Extrapolation
- Fatigue damage assessment
- Blade fatigue
- Multi-modal
- Frequency domain fatigue assessment