Insights into the aerodynamic response of a harmonic oscillating airfoil in various turbulent flows.

Yongfei Zhao, Mingshui Li, Yang Yang
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Abstract

The general theory of aerodynamic instability and the mechanism of flutter has been applied for decades in the environmental condition of uniform flow. Given the substantial growth in wind energy technology and aerospace in recent decades, there has been a greater focus on exploring the aerodynamic performance of oscillating airfoils in the environment of turbulence rather than just uniform flow. Most current research remains based on aerodynamic models obtained from potential flow theory, which have been thoroughly demonstrated through experimentation to be effective under the condition of uniform flow. However, it is still unclear whether turbulence and its interaction with the airfoil will cause traditional aerodynamic models to breakdown and how it will change under turbulent conditions. This study presents an analysis of how turbulence intensities and scale ratios individually influence the characteristics of oscillating airfoils. Furthermore, the turbulent kinetic energy and correlation are intimately associated with these two main components. The results suggest that as the turbulence intensities increase, more energy is injected, resulting in a larger amplitude of unsteady lift. In turbulence, smaller scale ratios reduce correlation and result in a decrease in the amplitude of lift. Turbulence could also lead to a departure of the transfer function from its theoretical value, known as the Theodorsen function. This work examines and evaluates the influence of turbulence on oscillating airfoils. The results might serve as a foundation for aerodynamic analysis to examine the stability of airfoils in turbulent flows.

洞察一个谐波振荡翼型在各种湍流的空气动力学响应。
气动不稳定性和颤振机理的一般理论已经在均匀流动环境下应用了几十年。鉴于近几十年来风能技术和航空航天的大幅增长,人们越来越关注于探索振荡翼型在湍流环境中的气动性能,而不仅仅是均匀流动环境。目前的研究大多是基于势流理论得到的气动模型,这些模型在均匀流动条件下的有效性已被实验充分证明。然而,目前尚不清楚湍流及其与翼型的相互作用是否会导致传统的空气动力学模型崩溃,以及在湍流条件下它将如何变化。本研究提出了湍流强度和尺度比如何单独影响振荡翼型特性的分析。此外,湍流动能和相关系数与这两个主要成分密切相关。结果表明,湍流强度越大,注入的能量越大,导致非定常升力幅值越大。在湍流中,较小的尺度比降低了相关性,导致升力幅度减小。湍流也可能导致传递函数偏离其理论值,即Theodorsen函数。这项工作检查和评估湍流对振荡翼型的影响。所得结果可作为气动分析的基础,以检验翼型在湍流中的稳定性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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