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中文核心期刊

超声速尾涡的稳定性分析

STABILITY ANALYSIS ON SUPERSONICTRAILING-LINE VORTEX

  • 摘要: 从N-S方程出发,通过正则模方法,研究了超声速尾涡的绝对/对流不稳定性性质.计算了流动的稳定性特征随马赫数M,周向波数n.,轴向自由流速度W0和旋转度q等流动参数的变化规律,找到了绝对/对流不稳定区域的边界.通过比较发现,马赫数的增加使流动由绝对不稳定向对流不稳定乃至稳定转化.在所计算的参数范围,周向波数的增加加速了这一转化过程,而且,轴向速度的增加,同样使流动向着稳定的方向转化.同时还分析了不同旋拧程度的流动受可压缩影响的不同.这些结果对于了解旋拧流动稳定性的物理机理以及进行流动控制都有着重要意义.

     

    Abstract: In recent years there has been a great deal of interests in the stability of swirlingflows. It is because of not only the significance to the enhancement of supersonic mixing butalso the important applications to many practical flows such as the trailing-line vortices behindan aircraft. The absolute/convective instability of incompressible swirling flows and the temporalinstability of compressible swirling flows have been fully explored, whereas the absolute/convectiveinstability of compressible swirling fl...

     

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