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Analysis of flutter effect in the pre-bending state of wind turbine blade
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Mu-en GAO1, Shi-tang KE1, 2, Hong-xin WU1, 2, Chun-wei ZHANG1, 2, Wen-xin TIAN1, Man-man LU1
Journal of Vibration Engineering | 2024, 37(6) : 986 - 996
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Journal of Vibration Engineering | 2024, 37(6): 986-996
Analysis of flutter effect in the pre-bending state of wind turbine blade
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Mu-en GAO1, Shi-tang KE1, 2, Hong-xin WU1, 2, Chun-wei ZHANG1, 2, Wen-xin TIAN1, Man-man LU1
Affiliations
  • 1Department of Civil and Airport Engineering,College of Civil Aviation,Nanjing University of Aeronautics and Astronautics,Nanjing 211106,China
  • 2Jiangsu Key Laboratory of Hi-Tech Research for Wind Turbine Design, Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China
Published: 2024-06-28 doi: 10.16385/j.cnki.issn.1004-4523.2024.06.009
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Most wind turbine blade pre-bending designs use the static aeroelastic analysis method. This approach often overlooks the aeroelastic coupling instability caused by the interaction of blade aerodynamic force,inertial force and elastic force. This oversight is particularly significant when considering flutter performance of ultra-long flexible blades of around 100 meters. To analyze the influence of different pre-bending sizes on flutter critical state of blade, aeroelastic model of the blade was designed based on the stiffness equivalence principle of the main beam. Wind tunnel tests revealed differences between the flutter interval and the critical wind speed of two pre-bending blades of a 15 MW wind turbine. Further analysis was conducted on four pre-bending blades using the corrected Blade Element Momentum Theory-Geometrically Exact Beam Theory (BEM-GEBT) coupling calculation method. This analysis compared and analyzed the flutter critical wind speed,aerodynamic force distribution and displacement spectrum characteristics of blades with different pre-bending sizes,revealing the flutter coupling modal mechanism. The research shows that the results of BEM-GEBT coupling calculation method align well with those of wind tunnel test. As the pre-bending size increases,the flutter critical wind speed of flap-edge coupling increases,and the flutter interval range remains essentially the same. The divergence rates of lift coefficient and pitching moment coefficient of different pre-bending blades are positively correlated with the displacement divergence rate. The average wind pressure curve shows significant changes in the pre-bending range of 3~4 m. The flap-edge coupling effect is larger than the flap-torsion coupling effect,and the flutter coupling frequency is dominated by the first-order flapwise frequency.

ultra-long flexible blades  /  pre-bending effect  /  wind tunnel test  /  aeroelastic coupling  /  flutter instability
Mu-en GAO, Shi-tang KE, Hong-xin WU, Chun-wei ZHANG, Wen-xin TIAN, Man-man LU. Analysis of flutter effect in the pre-bending state of wind turbine blade[J]. Journal of Vibration Engineering, 2024 , 37 (6) : 986 -996 . DOI: 10.16385/j.cnki.issn.1004-4523.2024.06.009
Year 2024 volume 37 Issue 6
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Article Info
doi: 10.16385/j.cnki.issn.1004-4523.2024.06.009
  • Receive Date:2022-01-29
  • Online Date:2026-02-09
  • Published:2024-06-28
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History
  • Received:2022-01-29
  • Revised:2022-05-03
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Affiliations
    1Department of Civil and Airport Engineering,College of Civil Aviation,Nanjing University of Aeronautics and Astronautics,Nanjing 211106,China
    2Jiangsu Key Laboratory of Hi-Tech Research for Wind Turbine Design, Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China
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表12种不同金属材料的力学参数

Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
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Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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