The temporal stability and growth characteristics of three-dimensional supersonic shear layers are numerically investigated. An explicit time-marching scheme that is second-order accurate in time and fourth-order accurate in space is used to study this problem. The shear layer is excited by instability waves computed from a linear stability analysis and random initial disturbances. At low convective Mach numbers, organized vortical structures develop both for the random disturbance and the modal disturbance cases. At supersonic convective Mach numbers, vortical structures develop initially but are not sustained in time. Temporal growth of disturbances is found to be a strong function of the convective Mach number
The paper is devoted to an experimental study of the laminar-turbulent transition and the instabilit...
A numerical investigation of the effects of nanosecond barrier discharge on the stability of a two-d...
AbstractSome general results on the stability of compressible shear flows are derived. It is shown t...
The effect of Mach number on the evolution of instabilities in the compressible mixing layer is inve...
We perform direct numerical simulations of transitional and developed turbulent shear flows. The ade...
A numerical model has been developed which simulates the three-dimensional stability and transition ...
Mixing layers are present in very different types of physical situations such as atmospheric flows, ...
The effect of Mach number on the plane muong layer has been investigated by means of linear stabilit...
The inviscid instability, with respect to supersonic disturbances of a spatially growing plane mixin...
The analysis of transition in fully three-dimensional boundary layers on high-speed aircraft is hamp...
The results of a numerical study of the development of periodic pulsations in a supersonic boundary ...
The late stages of transition to turbulence in a Mach two boundary layer are investigated by direct ...
The linear instability and breakdown to turbulence induced by an isolated roughnesselement in a boun...
Air flow in the wake region of a two-dimensional (plane) body with a blunt base has been studied usi...
A numerical method is given for direct numerical simulation of the nonlinear evolution of instabilit...
The paper is devoted to an experimental study of the laminar-turbulent transition and the instabilit...
A numerical investigation of the effects of nanosecond barrier discharge on the stability of a two-d...
AbstractSome general results on the stability of compressible shear flows are derived. It is shown t...
The effect of Mach number on the evolution of instabilities in the compressible mixing layer is inve...
We perform direct numerical simulations of transitional and developed turbulent shear flows. The ade...
A numerical model has been developed which simulates the three-dimensional stability and transition ...
Mixing layers are present in very different types of physical situations such as atmospheric flows, ...
The effect of Mach number on the plane muong layer has been investigated by means of linear stabilit...
The inviscid instability, with respect to supersonic disturbances of a spatially growing plane mixin...
The analysis of transition in fully three-dimensional boundary layers on high-speed aircraft is hamp...
The results of a numerical study of the development of periodic pulsations in a supersonic boundary ...
The late stages of transition to turbulence in a Mach two boundary layer are investigated by direct ...
The linear instability and breakdown to turbulence induced by an isolated roughnesselement in a boun...
Air flow in the wake region of a two-dimensional (plane) body with a blunt base has been studied usi...
A numerical method is given for direct numerical simulation of the nonlinear evolution of instabilit...
The paper is devoted to an experimental study of the laminar-turbulent transition and the instabilit...
A numerical investigation of the effects of nanosecond barrier discharge on the stability of a two-d...
AbstractSome general results on the stability of compressible shear flows are derived. It is shown t...