首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >NUMERICAL TESTING OF A TRAILING EDGE PASSIVE MORPHING CONTROL FOR LARGE AXIAL FAN BLADES
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NUMERICAL TESTING OF A TRAILING EDGE PASSIVE MORPHING CONTROL FOR LARGE AXIAL FAN BLADES

机译:大型轴流风扇叶片尾缘被动变形控制的数值测试

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The concept of morphing geometry to control and stabilize the flow has been proposed and applied in several aeronautic and wind turbine applications. We studied the effect of a similar passive system applied on an axial fan blade, analysing potential benefits and disadvantages associated to the passive coupling between fluid and structure dynamics. The present work completes a previous study made at the section level, giving a view also on the three-dimensional effects. We use the numerical computation to simulate the system which defines a complex fluid-structure interaction problem. In order to do that, an in-house finite element solver, already used in the previous study, is applied to solve the coupled dynamics.
机译:已经提出了使几何形状变形以控制和稳定流动的概念,并将其应用于几种航空和风力涡轮机应用中。我们研究了在轴流风扇叶片上应用类似的被动系统的效果,分析了与流体动力学和结构动力学之间的被动耦合相关的潜在利弊。本工作完成了先前在本节进行的研究,并给出了三​​维效应的观点。我们使用数值计算来模拟定义复杂的流固耦合问题的系统。为了做到这一点,以前的研究已经使用了内部有限元求解器来求解耦合动力学。

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