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首页> 外文期刊>Journal of Fluid Mechanics >Evolution of nonlinear processes in a hypersonic boundary layer on a sharp cone
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Evolution of nonlinear processes in a hypersonic boundary layer on a sharp cone

机译:尖锥上高超声速边界层中非线性过程的演化

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摘要

Nonlinear processes in a hypersonic boundary layer on a sharp cone are considered using, the bicoherence method. The experiments are performed for a Mach number M-x = 5.95 with introduction of artificial wave packets at the frequency of the second mode. It is shown that the basic mechanism of nonlinear interaction at the location of the maximum r.m.s. voltage fluctuation is the subharmonic resonance; all nonlinear interactions in the maximum r.m.s. voltage fluctuation layer are related to the second mode of disturbances; nonlinear processes above and below that layer are much more intense than those in it. The effect of artificial disturbances on nonlinear interaction's in the boundary layer is shown to be insignificant.
机译:使用双相干方法考虑了尖锥上高超声速边界层中的非线性过程。对于马赫数M-x = 5.95进行实验,并以第二模式的频率引入人造波包。结果表明,最大r.m.s位置处非线性相互作用的基本机理。电压波动是次谐波谐振;最大r.m.s.中的所有非线性相互作用电压波动层与扰动的第二模式有关。该层上方和下方的非线性过程比其中的非线性过程要强烈得多。人工扰动对边界层非线性相互作用的影响被证明是微不足道的。

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