Nonlinear Instability in the Region of Laminar-Turbulent Transition in Supersonic Three-Dimensional Flow over a Flat Plate

被引:0
|
作者
I. I. Lipatov
R. Ya. Tugazakov
机构
[1] Central Aerohydrodynamic Institute (TsAGI),
来源
Fluid Dynamics | 2018年 / 53卷
关键词
D O I
暂无
中图分类号
学科分类号
摘要
Direct numerical simulation is applied to obtain laminar-turbulent transition in supersonic flow over a flat plate. It is shown that, due to the nonlinear instability, Tollmien–Schlichting waves generated in the boundary layer lead to the formation of oblique disturbances in the flow. These represent a combination of compression and expansion waves, whose intensities can be two orders higher than that of external harmonic disturbances. The patterns of the three-dimensional flow over the plate are presented and the structures of the turbulent flat-plate boundary layers are described for the freestream Mach numbers M = 2 and 4.
引用
收藏
页码:285 / 295
页数:10
相关论文
共 50 条