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The analysis of pitching wing with elastic deformation

机译:弹性变形的俯仰翼分析

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摘要

In this paper, the thrust generation, the efficiency and the flow field of pitching wing with elastic deformation by fluid force are investigated numerically. The Navier-Stokes equation and the equation of elastic deformation are combined by using the Newton- Raphson method. Then, the calculation of flow field and deformation of elastic wing are carried out simultaneously. The thrust generated by an elastic wing exceeds the thrust of rigid wing with the increase of pitching frequency. Furthermore, the efficiency of pitching wing with appropriate elasticity becomes higher than that of rigid wing. Elastic deformation of wing increases the thrust component of fluid force, and the power needed for pitching motion decreases by deformation of wing. These are the main factors that improve the characteristics of thrust generation and the efficiency of elastic wing. The optimal values of flexural rigidity exist for both thrust generation and efficiency respectively. The pitching wing with the optimal value of flexural rigidity improves the characteristics of thrust generation and efficiency substantially.
机译:在本文中,在数值上研究推力生成,俯仰机翼具有弹性变形的俯仰翼的流动场。通过使用牛顿方法来组合Navier-Stokes方程和弹性变形的方程。然后,同时进行流场的计算和弹性翼的变形。弹性翼产生的推力超过斜翼的推力随着俯仰频率的增加而产生刚性翼的推力。此外,具有适当弹性的俯仰机翼的效率变得高于刚性翼的效率。机翼的弹性变形增加了流体力的推力分量,通过机翼变形减小了俯仰运动所需的功率。这些是改善推力生成特性和弹性翼效率的主要因素。弯曲刚度的最佳值分别存在于推力生成和效率。具有最佳弯曲刚度值的俯仰翼提高了推力生成和效率的特性。

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