Revisit of the oblique-breakdown regime in supersonic boundary layers and mechanism of the extra amplification of streak modes

Author:

Song Runjie1,Dong Ming12ORCID,Zhao Lei3ORCID

Affiliation:

1. State Key laboratory of Nonlinear Mechanics, Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190, China

2. Sino-Russian Mathematics Center, Peking University, Beijing 100871, China

3. Department of Mechanics, Tianjin University, Tianjin, 300072, China

Abstract

In the low-Mach-number supersonic boundary layers, the oblique-breakdown regime may be the most efficient route to trigger the laminar–turbulent transition, because the most unstable Mack first mode always appears as an oblique wave. In this paper, we revisit this issue by use of the nonlinear parabolized stability equation (NPSE) approach and particularly focus on the extra amplification of the streak mode generated by the direct interaction of the introduced oblique modes. This mechanism is then well explained based on the weakly nonlinear analysis, and its predictions on the evolution of the streak mode and the two-dimensional traveling-wave mode are quantitatively confirmed by the NPSE calculations. Additionally, the important role of the streak mode, leading to the secondary instability, on triggering the transition onset is identified.

Funder

National Natural Science Foundation of China

Strategic Priority Research Program, CAS

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

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