长短轴比对高速椭圆锥流向涡稳定性的影响

Effect of major-to-minor axis ratio on the stability of streamwise vortices over high-speed elliptic cone

  • 摘要: 长短轴比是影响锥型体高速飞行器边界层转捩特性的关键几何参数,尤其对流向涡这类三维边界层结构作用显著。为深入探究其影响机制,本研究通过直接求解Navier-Stokes方程获得层流基本流,应用二维全局稳定性分析(Bi-Global)方法获取稳定性特征,系统分析了椭圆锥在不同长短轴比下流向涡的失稳特性。其中,来流马赫数Ma = 6,来流温度T_\mathrme = 52 K,单位雷诺数Re_\rmunit=1.02\times10^7/m,壁温T_\mathrmw = 300 K。模型球头半径1 mm,短轴的半锥角7^\circ,长短轴比e分别为1.25、1.5、2.0和4.0。基本流的计算结果表明,长短轴比e = 1.25时,椭圆锥中心线会形成低速条带,当长短轴比增大到1.5时,低速条带两侧会卷曲形成蘑菇状流向涡结构。随着长短轴比进一步增大,流向涡展向卷曲程度增大,形成位置更靠近上游,沿流向的发展演化速度更快。稳定性分析的结果表明,当e = 1.25时,椭圆锥中心线的主导模态为对称的Mack模态。当长短轴比增大到1.5时,上游是Mack模态占主导,最大N值可到8。随着下游流向涡卷曲成蘑菇状,边界层中开始出现不稳定的外模态。其中法向剪切占据主导的对称Y模态增长速度最快,并且最可能诱发流向涡转捩,其主导频率为179 kHz。随着模型长短轴比增大到4.0,展向剪切主导的Z模态增长率最大,最可能诱发流向涡转捩的模态由Y模态转变为Z模态。此外,基于\rme^N方法的转捩预测结果表明,长短轴比越大,计算域内积分得到的N值越大。这表明长短轴比越大,流向涡转捩位置越靠近上游,与流向涡形成规律一致。

     

    Abstract: The major-to-minor axis ratio is a key geometric parameter affecting boundary-layer transition on conical high-speed vehicles, with a particularly pronounced influence on three-dimensional boundary-layer structures such as streamwise vortices. To explore the underlying mechanisms, this study obtains the base-flow by directly solving the Navier–Stokes equations, and employs two-dimensional global stability analysis (Bi-Global) to systematically investigate the instability characteristics of streamwise vortices over an elliptic cone at various major-to-minor axis ratios. The freestream Mach number is 6, the static temperature is T_\mathrme = 52 K, the unit Reynolds number is Re_\rmunit=1.02\times10^7/m, and the wall temperature is T_\mathrmw = 300 K. The model has a nose radius of 1 mm, a semi-cone angle of 7^\circ along the minor axis, and major-to-minor axis ratios e of 1.25, 1.5, 2.0, and 4.0. The base-flow results show that at e=1.25, a low-speed streak forms along the centerline of the elliptic cone. When the major-to-minor axis ratio increases to 1.5, the low-speed streak rolls up on both sides, giving lift-up to mushroom-shaped streamwise vortices. As the ratio increases further, the spanwise rolling-up of the streamwise vortices becomes more intense, their formation shifts upstream, and their streamwise development and evolution accelerate. Stability analysis reveals that at e=1.25, the dominant mode along the centerline is the symmetric Mack mode. When the ratio increases to 1.5, the Mack mode dominates upstream, with a maximum N factor reaching 8. Further downstream, as the streamwise vortices roll up into mushroom shapes, unstable outer modes emerge in the boundary layer. Among these, the symmetric Y mode, dominated by wall-normal shear, exhibits the highest growth rate and is most likely to trigger transition of the streamwise vortices, with a dominant frequency of 179 kHz. When the major-to-minor axis ratio increases to 4.0, the Z mode, dominated by spanwise shear, becomes the fastest-growing mode, and the mode most likely to induce transition shifts from the Y mode to the Z mode. Transition prediction based on the \rme^N method shows that a larger major-to-minor axis ratio yields a higher integrated N factor within the computational domain. This indicates that the larger the major-to-minor axis ratio, the farther upstream the streamwise vortex transition occurs, which is consistent with the formation characteristics of the streamwise vortices.

     

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