Details
Original language | English |
---|---|
Article number | 052083 |
Pages (from-to) | 1-9 |
Number of pages | 9 |
Journal | Journal of Physics: Conference Series |
Volume | 2020 |
Issue number | 1618 |
Publication status | Published - 22 Sept 2020 |
Event | Science of Making Torque from Wind 2020, TORQUE 2020 - Virtual, Online, Netherlands Duration: 28 Sept 2020 → 2 Oct 2020 |
Abstract
Keywords
- aeroelastic stability, instability, flutter, wind turbine, stability, code-to-code, code to code, OpenFAST, HAWC2, GH Bladed, Simpack, alaska
ASJC Scopus subject areas
- Physics and Astronomy(all)
- General Physics and Astronomy
Sustainable Development Goals
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In: Journal of Physics: Conference Series, Vol. 2020, No. 1618, 052083, 22.09.2020, p. 1-9.
Research output: Contribution to journal › Article › Research › peer review
}
TY - JOUR
T1 - Wind turbine stability: Comparison of state-of-the-art aeroelastic simulation tools
AU - Hach, O.
AU - Verdonck, H.
AU - Polman, J. D.
AU - Balzani, C.
AU - Müller, S.
AU - Rieke, J.
AU - Hennings, H.
N1 - Funding Information: This work is a collaboration of four partners from research and industry in the frame of work package 4.2 of the German national research project SmartBlades2. This project is funded by the German Federal Ministry for Economic Affairs and Energy, grant no. 0324032 A/C.
PY - 2020/9/22
Y1 - 2020/9/22
N2 - As rotor diameters and blade flexibility are increasing, current and future generation wind turbines are more susceptible to aeroelastic instabilities. It is thus important to know the prediction capabilities of state-of-the-art simulation tools in regards of the onset of aeroelastic instability. This article presents results of a code-to-code comparison of five different simulation codes using a representative wind turbine model. It is shown that the models are in good agreement in terms of isolated structural dynamics and steady state aeroelastics. The more complex the test cases become, the more significant are the differences in the results. In the final step of comparison, the aeroelastic stability limit is determined through a runaway analysis. The instability onset is predicted at different wind speeds and the underlying mechanisms differ between the tools. A Campbell diagram is used to correlate the findings of time domain simulation tools with those of a linear analysis in the frequency domain.
AB - As rotor diameters and blade flexibility are increasing, current and future generation wind turbines are more susceptible to aeroelastic instabilities. It is thus important to know the prediction capabilities of state-of-the-art simulation tools in regards of the onset of aeroelastic instability. This article presents results of a code-to-code comparison of five different simulation codes using a representative wind turbine model. It is shown that the models are in good agreement in terms of isolated structural dynamics and steady state aeroelastics. The more complex the test cases become, the more significant are the differences in the results. In the final step of comparison, the aeroelastic stability limit is determined through a runaway analysis. The instability onset is predicted at different wind speeds and the underlying mechanisms differ between the tools. A Campbell diagram is used to correlate the findings of time domain simulation tools with those of a linear analysis in the frequency domain.
KW - aeroelastic stability
KW - instability
KW - flutter
KW - wind turbine
KW - stability
KW - code-to-code
KW - code to code
KW - OpenFAST
KW - HAWC2
KW - GH Bladed
KW - Simpack
KW - alaska
UR - http://www.scopus.com/inward/record.url?scp=85108989203&partnerID=8YFLogxK
U2 - 10.1088/1742-6596/1618/5/052048
DO - 10.1088/1742-6596/1618/5/052048
M3 - Article
VL - 2020
SP - 1
EP - 9
JO - Journal of Physics: Conference Series
JF - Journal of Physics: Conference Series
SN - 1742-6588
IS - 1618
M1 - 052083
T2 - Science of Making Torque from Wind 2020, TORQUE 2020
Y2 - 28 September 2020 through 2 October 2020
ER -