Energy Transfer Mechanisms in Wake-Modulated Transonic Flutter
尾流调制跨声速颤振中的能量传递机制
Vedasri Godavarthi, Jacob Turner, Jung-Hee Seo, Rajat Mittal
AI总结 通过高保真直接数值模拟和能量图,研究了尾流扰动对跨声速颤振的影响,发现圆柱体显著扩大颤振边界,并利用力分解方法识别出机翼与圆柱之间的间隙流是能量传递的主要来源。
Comments 26 pages, 16 figures
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跨声速颤振是一种有害的气动弹性不稳定性,可产生大幅结构振荡,导致严重振动、疲劳损伤、运行极限降低,甚至灾难性结构失效。来流尾流扰动会进一步加剧这种不稳定性,因此识别预测和控制颤振起始的底层气动机制至关重要。其底层流动物理复杂,涉及尾流与机翼的非线性相互作用、激波运动、激波诱导流动分离、涡脱落以及机翼运动。在本研究中,我们对带有下翼圆柱的NACA0012翼型在正弦俯仰运动下进行了高保真直接数值模拟,涉及不同跨声速马赫数和雷诺数10,000。通过能量图,我们发现与仅翼型系统相比,添加圆柱体显著扩大了颤振边界。我们将力分解方法扩展到可压缩流中,分解流动与翼型之间的功率传递。将该方法应用于流动域的不同区域表明,机翼与圆柱之间的间隙流是流动向翼型能量传递的主要贡献者。圆柱体的阻塞效应导致机翼上的流动加速,进一步增强了颤振趋势。我们研究了圆柱体相对于翼型的位置,发现只有当圆柱体放置在翼型枢轴点上游时,颤振才会增强。当前研究突出了这种分解方法如何解析复杂非定常高速流中的力和能量传递机制。
Transonic flutter is a detrimental aeroelastic instability that can generate large-amplitude structural oscillations, leading to severe vibration, fatigue damage, reduced operational limits, and potentially catastrophic structural failure. Incoming wake disturbances can further amplify this instability, making it critical to identify the underlying aerodynamic mechanisms responsible for predicting and controlling flutter onset. The underlying flow physics is complex with nonlinear interactions between the wake and the wing, shock motion, shock-induced flow separation, vortex shedding and the wing motion. In this study, we perform high-fidelity direct numerical simulations of a sinusoidally pitching NACA0012 airfoil with an underwing cylinder at various transonic Mach numbers and a Reynolds number of 10,000. Through energy maps, we identify that the addition of the cylinder significantly expands flutter boundaries compared to an airfoil-only system. We extend the force partitioning method to partition the power transferred between the flow and the airfoil for compressible flows. Application of this approach to distinct regions of the flow domain indicates that the gap flow between the wing and the cylinder is the dominant contributor to the energy transfer from flow to the wing. The blockage effects due to the cylinder cause flow acceleration on the wing which further enhances the tendency for flutter. We investigate cylinder placement relative to the airfoil to reveal that flutter is enhanced only when the cylinder is placed upstream of the pivot point on the airfoil. The current study highlights how such partitioning methods can parse force and energy transfer mechanisms in complex, unsteady high-speed flows.