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不可压平板边界层转捩机理

李宁 罗纪生

李宁, 罗纪生. 不可压平板边界层转捩机理[J]. 航空动力学报, 2013, 28(4): 743-751.
引用本文: 李宁, 罗纪生. 不可压平板边界层转捩机理[J]. 航空动力学报, 2013, 28(4): 743-751.
LI Ning, LUO Ji-sheng. Transition mechanism of an incompressible boundary layer on a flat plate[J]. Journal of Aerospace Power, 2013, 28(4): 743-751.
Citation: LI Ning, LUO Ji-sheng. Transition mechanism of an incompressible boundary layer on a flat plate[J]. Journal of Aerospace Power, 2013, 28(4): 743-751.

不可压平板边界层转捩机理

基金项目: 国家自然科学基金(10632050)

Transition mechanism of an incompressible boundary layer on a flat plate

  • 摘要: 基于扰动形式N-S方程,从空间模式的角度,采用Fourier伪谱及MPI(massage passing interface)并行方法,模拟了不可压平板边界层从层流到湍流的转捩过程.通过对计算统计数据的分析,比较了不同幅值入口扰动引起的转捩过程的同异.研究结果表明:当层流中扰动幅值逐渐增大后,非线性作用将修正平均流剖面,表现为不稳定区域逐渐扩大,很多高次谐波被激发.当平均流剖面被修正到一定程度时,不稳定区域变得很大,这使得更多的高次谐波被快速激发并迅速增长,即转捩过程开始.由于大量谐波快速增长导致扰动能量快速增长,同时,扰动能量的快速增长又进一步加速了平均流剖面的快速修正,即平均流剖面的不稳定特性发生了改变,这样的相互作用使得层流快速变为湍流,因此,平均流剖面不稳定特性的改变在转捩过程中起到了关键作用.

     

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出版历程
  • 收稿日期:  2012-09-24
  • 刊出日期:  2013-04-28

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