高超声速6°迎角圆锥边界层背风流向涡稳定性分析

Stability analyses of leeward streamwise vortices for a hypersonic yawed cone at 6 degree angle of attack

  • 摘要: 针对马赫数6、迎角6°圆锥边界层背风面流向涡开展了直接数值模拟和稳定性分析,其中,稳定性分析工具包括空间BiGlobal方法和面推进的PSE3D方法。研究发现,有迎角圆锥边界层背风中心线附近会自发形成一对对转的强流向涡。这对流向涡或因低频反对称模态和高频对称模态的共同作用而在下游破碎。

     

    Abstract: The stability of leeward streamwise vortices over a Mach 6 yawed cone with 6 degree angle of attack is investigated by using direct numerical simulation (DNS) and stability analyses including spatial BiGlobal and plane-marching parabolized stability equations (PSE3D). It is found that a pair of strong streamwise vortices inducing low-speed mushroom structure simultaneously emerge in the vicinity of the leeward plane. Theoretical results indicate that both low-frequency sinuous modes and high-frequency varicose modes may play an important role in the breakdown of the streamwise vortices.

     

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