Add to ORKGThe paper is devoted to an experimental study of the laminar-turbulent transition in a self-similar boundary layer with an adverse pressure gradient (APG). The main attention is paid to dominating mechanisms of weakly-nonlinear interactions between the wide-band frequency-wavenumber spectrum of Tollmien – Schlichting (TS) waves (i.e. the noise-like instabilit
International audienceThe interaction of an oblique shock wave and a laminar boundary layer developi...
An experimental and theoretical investigation has been carried out to understand the tonal noise gen...
The structure of wall pressure fluctuations beneath a turbulent boundary layer interacting with a no...
A new method of experimental study of late nonlinear stages of laminar-turbulent transition is devel...
The airfoil self-noise phenomenon is present in several applications of societal relevance, such as ...
The problem of the excitation of own modes by disturbances of a free-stream flow has been solved in ...
Linear stability analysis (LSA) of a self-similar adverse pressure gradient (APG) turbulent boundary...
Transition to turbulence in incompressible adverse-pressure-gradient (APG) boundary layers is invest...
This is an account of an inr&”gation in which oscillations were disco~red in the laminar boundar...
Acoustic plane waves were shown to excite Tollmien-Schlichting (T-S) waves in a flat plate laminar b...
The roles of weakly nonlinear triad interactions and the self-interaction of primary instabilities i...
AbstractThe influence of spanwise perturbations on the transition to turbulence of a strong adverse ...
We present direct numerical simulations of the spatial development of a triad of normal mode perturb...
As a first step towards understanding the role of free-stream turbulence in laminar–turbulent transi...
A low-turbulence subsonic wind tunnel was used to study the influence of acoustic disturbances on th...
International audienceThe interaction of an oblique shock wave and a laminar boundary layer developi...
An experimental and theoretical investigation has been carried out to understand the tonal noise gen...
The structure of wall pressure fluctuations beneath a turbulent boundary layer interacting with a no...
A new method of experimental study of late nonlinear stages of laminar-turbulent transition is devel...
The airfoil self-noise phenomenon is present in several applications of societal relevance, such as ...
The problem of the excitation of own modes by disturbances of a free-stream flow has been solved in ...
Linear stability analysis (LSA) of a self-similar adverse pressure gradient (APG) turbulent boundary...
Transition to turbulence in incompressible adverse-pressure-gradient (APG) boundary layers is invest...
This is an account of an inr&”gation in which oscillations were disco~red in the laminar boundar...
Acoustic plane waves were shown to excite Tollmien-Schlichting (T-S) waves in a flat plate laminar b...
The roles of weakly nonlinear triad interactions and the self-interaction of primary instabilities i...
AbstractThe influence of spanwise perturbations on the transition to turbulence of a strong adverse ...
We present direct numerical simulations of the spatial development of a triad of normal mode perturb...
As a first step towards understanding the role of free-stream turbulence in laminar–turbulent transi...
A low-turbulence subsonic wind tunnel was used to study the influence of acoustic disturbances on th...
International audienceThe interaction of an oblique shock wave and a laminar boundary layer developi...
An experimental and theoretical investigation has been carried out to understand the tonal noise gen...
The structure of wall pressure fluctuations beneath a turbulent boundary layer interacting with a no...