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Numerical Analysis of theWall Effect on Flow Around Airfoil Subjected to a Pitching Movement

机译:俯仰运动对翼型绕流影响的数值分析

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摘要

In this work, we discuss the problem of the flow around a NACA0012 airfoil subjected to a pitching movement. The set of flow equations coupled with solid movement is solved with a finite element method using ANSYS program. Results show that our numerical model presents a good agreement in comparison with the experimental and the numerical results available in the literature. Next, the airfoil pitching movement is analyzed with the presence of the wall in the flow. It is shown that, the wall has a significant effect on aerodynamic parameters of airfoil. It found that the wall slows down the flow.
机译:在这项工作中,我们讨论了围绕俯仰运动的NACA0012机翼周围的流动问题。使用ANSYS程序通过有限元方法求解与固体运动相关的流动方程组。结果表明,与文献中的实验结果和数值结果相比,我们的数值模型具有很好的一致性。接下来,在流中存在壁的情况下分析翼型俯仰运动。结果表明,该壁对翼型的空气动力学参数具有显着影响。发现墙使流动减慢了。

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