The paper describes experiments on acoustically excited axisymmetric turbulent jet flows. The investigation is based on the hypothesis that so called oblique transition may play a role in the breakdown to turbulence for an axisymmetric jet. For wall bounded flows oblique transition gives rise to steady streamwise streaks that break down to turbulence, as for instance documented by Elofsson & Alfredsson (J. Fluid Mech. 358). The scenario of oblique transition has so far not been considered for jet flows and the aim was to study the effect of two oblique modes on the transition scenario as well as on the flow dynamics. Even though it was not possible to detect the presence of streamwise streaks, for a certain range of the excitation frequ...
© 2017 American Physical Society. We investigate the effect of nonlinearities on the frequency respo...
International audienceThe effect of an external excitation on circular impinging jet flow is studied...
In the low-Mach-number supersonic boundary layers, the oblique-breakdown regime may be the most effi...
The paper describes experiments on acoustically excited axisymmetric turbulent jet flows. The invest...
none4noneA. Segalini; R. Orlu; A. Talamelli; P.H. AlfredssonA. Segalini; R. Orlu; A. Talamelli; P.H....
none4For many years investigations have been conducted to understand the flow instabilities that lea...
none4Coaxial jets are used in many technological applications such as burners, turbofans, etc. They ...
Traditional research on laminar-turbulent transition has focused on scenarios that are caused by the...
The evolution of the large scale structures and the mean field were investigated in axisymmetric and...
A modal spectrum technique was used to study coherent instability modes (both axisymmetric and azimu...
The structure of an axisymmetric jet in the near field is discussed for jet noise and for jet imping...
This thesis deals with the description and development of two classical turbulent shear flows, namel...
Typescript (photocopy).An acoustically excited (St = 0.50), Mach 0.15, axisymmetric free jet operati...
Shear-layer instabilities of a pulsed stack-issued transverse jet were studied experimentally in a w...
This paper presents the results of an experimental investigation performed about the entrainment phe...
© 2017 American Physical Society. We investigate the effect of nonlinearities on the frequency respo...
International audienceThe effect of an external excitation on circular impinging jet flow is studied...
In the low-Mach-number supersonic boundary layers, the oblique-breakdown regime may be the most effi...
The paper describes experiments on acoustically excited axisymmetric turbulent jet flows. The invest...
none4noneA. Segalini; R. Orlu; A. Talamelli; P.H. AlfredssonA. Segalini; R. Orlu; A. Talamelli; P.H....
none4For many years investigations have been conducted to understand the flow instabilities that lea...
none4Coaxial jets are used in many technological applications such as burners, turbofans, etc. They ...
Traditional research on laminar-turbulent transition has focused on scenarios that are caused by the...
The evolution of the large scale structures and the mean field were investigated in axisymmetric and...
A modal spectrum technique was used to study coherent instability modes (both axisymmetric and azimu...
The structure of an axisymmetric jet in the near field is discussed for jet noise and for jet imping...
This thesis deals with the description and development of two classical turbulent shear flows, namel...
Typescript (photocopy).An acoustically excited (St = 0.50), Mach 0.15, axisymmetric free jet operati...
Shear-layer instabilities of a pulsed stack-issued transverse jet were studied experimentally in a w...
This paper presents the results of an experimental investigation performed about the entrainment phe...
© 2017 American Physical Society. We investigate the effect of nonlinearities on the frequency respo...
International audienceThe effect of an external excitation on circular impinging jet flow is studied...
In the low-Mach-number supersonic boundary layers, the oblique-breakdown regime may be the most effi...