首页> 外文会议>Robotics and Automation, 2004. Proceedings. ICRA '04. 2004 IEEE International Conference on >Free-flight analysis of flapping flight during turning by fluid-structure interaction finite element analysis based on arbitrary Lagrangian-Eulerian method
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Free-flight analysis of flapping flight during turning by fluid-structure interaction finite element analysis based on arbitrary Lagrangian-Eulerian method

机译:基于任意拉格朗日-欧拉方法的流固耦合有限元分析

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An insect's flapping flight is an attractive method of transportation. It shows many useful flight modes such as maneuverable turning and stable hovering. In recent studies, experimental methods and numerical simulations have been successfully applied to solve the mechanism quantitatively. However, it is extremely difficult to accurately estimate the deformation of the wing caused by interaction with airflow. In prior studies, we analyzed this problem using a novel numerical simulation, fluid-structure interaction analysis, in order to represent this interactive behavior accurately, and achieved the quantitative evaluation of dragonfly hovering with flexible wings. As an advanced analysis, we added a solution of the interaction between the body and wings to the method, and realized free-flight simulation. Here, we demonstrate a sharp turn of 10 rad/s in a numerical simulation using a model based on an actual dragonfly.
机译:昆虫的拍打飞行是一种有吸引力的运输方法。它显示了许多有用的飞行模式,例如可操纵的转弯和稳定的悬停。在最近的研究中,实验方法和数值模拟已成功地应用于定量地解决该机理。但是,很难准确地估计由于与气流相互作用而引起的机翼变形。在先前的研究中,我们使用新颖的数值模拟,流固耦合分析来分析此问题,以便准确地表示这种交互行为,并实现了带有柔性翼的蜻蜓盘旋的定量评估。作为高级分析,我们在该方法中添加了身体与机翼之间相互作用的解决方案,并实现了自由飞行仿真。在这里,我们使用基于实际蜻蜓的模型在数值模拟中演示了10 rad / s的急转弯。

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