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VORTEX SHEDDING LOCK-IN DUE TO STREAM-WISE OSCILLATION OF A 2-D WIND TURBINE BLADE SECTION AT HIGH ANGLES OF ATTACK.

机译：由于在高角度攻击下二维风力涡轮机叶片的流动振动，导致涡旋式切入锁定。

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Alberto Pellegrino; Craig Meskell;
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1. Vortex Shedding Lock-In due to Pitching Oscillation of a Wind Turbine Blade Section at High Angles of Attack [J] . Meskell Craig, Pellegrino Alberto International journal of aerospace engineering . 2019,第PTa1期

机译：风力涡轮机叶片部分在高攻角下的俯仰振荡会导致涡旋脱落锁定
2. Vortex Shedding Lock-In due to Pitching Oscillation of a Wind Turbine Blade Section at High Angles of Attack [J] . Meskell Craig, Pellegrino Alberto International journal of aerospace engineering . 2019,第PTa1期

机译：由于在高角度的攻击角度下，涡旋脱落锁定锁定锁定
3. Vortex Shedding Lock-In due to Pitching Oscillation of a Wind Turbine Blade Section at High Angles of Attack [J] . Craig Meskell, Alberto Pellegrino International journal of aerospace engineering . 2019,第4期

机译：由于在高角度的攻击角度下，涡旋脱落锁定锁定锁定
4. VORTEX SHEDDING LOCK-IN DUE TO STREAM-WISE OSCILLATION OF A 2-D WIND TURBINE BLADE SECTION AT HIGH ANGLES OF ATTACK [C] . Alberto Pellegrino, Craig Meskell ASME Pressure Vessels and Piping conference . 2014

机译：二维风轮机叶片在高攻角下的明智振荡，从而使涡旋切入锁定
5. Power generation using lock-in vortex shedding frequencies from quasi-constant airflow. [D] . Nayyar, Abhishek. 2015

机译：使用准恒定气流中的锁定涡旋脱落频率进行发电。
6. Full-Scale Fatigue Testing of a Wind Turbine Blade in Flapwise Direction and Examining the Effect of Crack Propagation on the Blade Performance [O] . Othman Al-Khudairi, Homayoun Hadavinia, Christian Little, 2017

机译：风力涡轮机叶片沿翼展方向的全尺寸疲劳测试并研究裂纹扩展对叶片性能的影响
7. VORTEX SHEDDING LOCK-IN DUE TO STREAM-WISE OSCILLATION OF A 2-D WIND TURBINE BLADE SECTION AT HIGH ANGLES OF ATTACK. [O] . Alberto Pellegrino, Craig Meskell 2015

机译：由于在高角度攻击下二维风力涡轮机叶片的流动振动，导致涡旋式切入锁定。
8. An Experimental Investigation of Steady Asymmetric Vortex Shedding from a Slender Body of Revolution at High Angles of Attack. [R] . turelli,robert rudolph 1977

机译：高攻角下细长体转动稳态不对称涡旋脱落的实验研究。

VORTEX SHEDDING LOCK-IN DUE TO STREAM-WISE OSCILLATION OF A 2-D WIND TURBINE BLADE SECTION AT HIGH ANGLES OF ATTACK.

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