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Investigations of aerodynamic drag forces during structural blade testing using high-fidelity fluid–structure interaction

机译:使用高保真流体结构相互作用在结构刀片测试期间的空气动力学阻力的研究

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Aerodynamic loads need to be known for planning and defining test loads beforehand for wind turbine blades that are tested for fatigue certifications. It is known that the aerodynamic forces, especially drag, are different for tests and operation, due to the entirely different flow conditions. In test facilities, a vibrating blade will move in and out of its own wake, increasing the drag forces on the blade. This is not the case in operation. To study this special aerodynamic condition present during experimental tests, numerical simulations of a wind turbine blade during pull–release tests were conducted. High-fidelity three-dimensional computational fluid dynamics methods were used throughout the simulations. In this way, the fluid mechanisms and their impact on the moving blade are clarified, and through the coupling with a structural solver, the fluid–structure interaction is studied. Results are compared to actual measurements from experimental tests, verifying the approach. It is found that the blade experiences a high drag due to its motion towards its own whirling wake, resulting in an effective drag coefficient of approximately 5.3?for the 90° angle of attack. This large drag coefficient was implemented in a fatigue test load simulation, resulting in a significant decrease in bending moment along the blade, leading to less load being applied than intended. The confinement from the test facility did not impact this specific test setup, but simulations with longer blades could possibly yield different conclusions. To the knowledge of the authors, this investigation, including three-dimensional effects, structural coupling and confinement, is the first of its kind.
机译:需要了解空气动力学载荷,以便预先为疲劳认证测试的风力涡轮机叶片规划和定义测试负载。众所周知,由于完全不同的流动条件,空气动力,尤其是拖曳,尤其是对测试和操作的不同。在测试设施中,振动刀片将进出自己的尾迹,增加刀片上的拖曳力。操作中不是这种情况。为了研究在实验测试期间存在的这种特殊的空气动力学条件,进行了拉释试验期间风力涡轮机叶片的数值模拟。在整个模拟中使用高保真三维计算流体动力学方法。以这种方式,阐明了流体机构及其对移动刀片的撞击,并通过与结构求解器的联接,研究了流体结构相互作用。结果与实验测试的实际测量相比,验证了这种方法。发现刀片由于其运动朝向其自身的旋转唤醒而经历了高拖动,导致有效的拖动系数约为5.3?对于90°攻角。该大型阻力系数在疲劳试验负载模拟中实现,导致沿着叶片的弯矩显着降低,导致较少的负载较少。从测试设施的监禁没有影响这个特定的测试设置,但具有更长刀片的模拟可能产生不同的结论。为了提交作者的知识,这项调查,包括三维效果,结构耦合和禁闭,是首先。

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