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Three-Wave Interactions between Disturbances in the Hypersonic Boundary Layer on Impermeable and Porous Surfaces

机译:不可渗透和多孔表面高超声速边界层中扰动之间的三波相互作用

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The interaction between disturbances in the hypersonic boundary layer on impermeable and porous surfaces is considered within the framework of weakly-nonlinear stability theory. It is established that on the impermeable surface nonlinear interactions between different waves (acoustic and vortex) occur in the parametric resonance regime. The role of pumping wave is played by a plane acoustic wave. The nonlinear interactions take place over a wide frequency range and can lead to the packet growth of Tollmien-Schlichting waves. On the porous surface the analogous interactions are fairly weak and result in a slight decay of the acoustic mode and a slight amplification of the vortex mode. This leads to the dragging out of the laminar flow regime and the regions of linear disturbance growth. In this situation the low-frequency spectrum of the vortex modes may be filled on account of the nonlinear processes occurring in the three-wave systems between the vortex components.
机译:在弱非线性稳定性理论的框架内,考虑了高渗超音速边界层在不透水和多孔表面扰动之间的相互作用。可以确定的是,在不可渗透的表面上,不同的波(声学波和涡旋波)之间的非线性相互作用会发生在参数共振状态下。平面声波起着泵浦波的作用。非线性相互作用发生在很宽的频率范围内,并可能导致托尔米-施利希廷波的包增长。在多孔表面上,类似的相互作用非常弱,导致声模略有衰减,涡模略有放大。这导致层流状态和线性扰动增长区域被拖出。在这种情况下,由于在涡流分量之间的三波系统中发生的非线性过程,涡流模式的低频频谱可能被填充。

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