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 t...
We study the spatial instability of a pair of symmetric oblique modes in the long-wave limit using m...
The effect of Mach number on the growth of unstable disturbances in a boundary layer undergoing a st...
Contrary to incompressible flows, there has been an immense research gap in the flow transition cont...
In the low-Mach-number supersonic boundary layers, the oblique-breakdown regime may be the most effi...
In this paper, we present a systematic study of the nonlinear evolution of the travelling Mack modes...
Optimal initial conditions for transient growth in a two-dimensional boundary layer flow correspond ...
The nal stage of transition to turbulence in a supersonic at-plate boundary layer at Mach 3 is inve...
Traditional research on laminar-turbulent transition has focused on scenarios that are caused by the...
AbstractStability of a supersonic boundary layer over two-dimensional smooth humps with their height...
Abstract The nonlinear analyses of the hypersonic and high-enthalpy boundary-layer transition had re...
The late stages of transition to turbulence in a Mach two boundary layer are investigated by direct ...
The evolution of Görtler vortices and its interaction with other instabilities are investigated in t...
Parabolized stability equations (PSE) are used in a variational approach to study the optimal, non-m...
AbstractThis article studies the nonlinear evolution of disturbance waves in supersonic nonparallel ...
AbstractThe evolution of Görtler vortices and its interaction with other instabilities are investiga...
We study the spatial instability of a pair of symmetric oblique modes in the long-wave limit using m...
The effect of Mach number on the growth of unstable disturbances in a boundary layer undergoing a st...
Contrary to incompressible flows, there has been an immense research gap in the flow transition cont...
In the low-Mach-number supersonic boundary layers, the oblique-breakdown regime may be the most effi...
In this paper, we present a systematic study of the nonlinear evolution of the travelling Mack modes...
Optimal initial conditions for transient growth in a two-dimensional boundary layer flow correspond ...
The nal stage of transition to turbulence in a supersonic at-plate boundary layer at Mach 3 is inve...
Traditional research on laminar-turbulent transition has focused on scenarios that are caused by the...
AbstractStability of a supersonic boundary layer over two-dimensional smooth humps with their height...
Abstract The nonlinear analyses of the hypersonic and high-enthalpy boundary-layer transition had re...
The late stages of transition to turbulence in a Mach two boundary layer are investigated by direct ...
The evolution of Görtler vortices and its interaction with other instabilities are investigated in t...
Parabolized stability equations (PSE) are used in a variational approach to study the optimal, non-m...
AbstractThis article studies the nonlinear evolution of disturbance waves in supersonic nonparallel ...
AbstractThe evolution of Görtler vortices and its interaction with other instabilities are investiga...
We study the spatial instability of a pair of symmetric oblique modes in the long-wave limit using m...
The effect of Mach number on the growth of unstable disturbances in a boundary layer undergoing a st...
Contrary to incompressible flows, there has been an immense research gap in the flow transition cont...