首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >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:大型轴流风机叶片后缘无源变形控制的数值测试

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摘要

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, analyzing 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 (3D) effects. We use the numerical computation to simulate the system, which defines a complex fluid–structure interaction (FSI) problem. In order to do that, an in-house finite element (FE) 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被动系统的效果,分析了流体和结构动力学之间被动耦合的潜在利弊。本工作完成了以前在部分级别进行的研究,并提供了有关三维(3D)效果的观点。我们使用数值计算来模拟系统,该系统定义了复杂的流固耦合(FSI)问题。为了做到这一点,在先前的研究中已经使用的内部有限元(FE)求解器被用于求解耦合动力学。

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