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On the nonlinear stability of a high-speed, axisymmetric boundary layer

机译:高速轴对称边界层的非线性稳定性

摘要

The stability of a high-speed, axisymmetric boundary layer is investigated using secondary instability theory and direct numerical simulation. Parametric studies based on the temporal secondary instability theory identify subharmonic secondary instability as a likely path to transition on a cylinder at Mach 4.5. The theoretical predictions are validated by direct numerical simulation at temporally-evolving primary and secondary disturbances in an axisymmetric boundary-layer flow. At small amplitudes of the secondary disturbance, predicted growth rates agree to several significant digits with values obtained from the spectrally-accurate solution of the compressible Navier-Stokes equations. Qualitative agreement persists to large amplitudes of the secondary disturbance. Moderate transverse curvature is shown to significantly affect the growth rate of axisymmetric second mode disturbances, the likely candidates of primary instability. The influence of curvature on secondary instability is largely indirect but most probably significant, through modulation of the primary disturbance amplitude. Subharmonic secondary instability is shown to be predominantly inviscid in nature, and to account for spikes in the Reynolds stress components at or near the critical layer.
机译:利用二次不稳定性理论和直接数值模拟研究了高速轴对称边界层的稳定性。基于时间次级不稳定性理论的参数研究将次谐波次级不稳定性视为在4.5马赫数的圆柱上过渡的可能路径。理论预测通过在轴对称边界层流中随时间演化的一次扰动和二次扰动的直接数值模拟得到验证。在较小的二次扰动幅度下,预测的增长率与从可压缩的Navier-Stokes方程的频谱精确解中获得的值一致,为几个有效数字。定性一致性持续存在于较大的二次干扰幅度中。研究表明,适度的横向曲率会显着影响轴对称第二模式扰动的增长速度,而第二对称模式扰动可能是主要的不稳定因素。曲率对次级不稳定性的影响在很大程度上是间接的,但很可能是通过调制初级干扰幅度而产生的。次谐波次要不稳定性在自然界中主要表现为无形,并解释了关键层或附近的雷诺应力分量的峰值。

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