The hydrodynamic instability in an industrial, two-staged, counter-rotative, swirled injector of highly complex geometry is under investigation. Large eddy simulations (LES) show that the complicated and strongly nonparallel flow field in the injector is superimposed by a strong precessing vortex core (PVC). Mean flow fields of LES, validated by experimental particle image velocimetry (PIV) measurements, are used as input for both local and global linear stability analysis (LSA). It is shown that the origin of the instability is located at the exit plane of the primary injector. Mode shapes of both global and local LSA are compared to dynamic mode decomposition (DMD) based on LES snapshots, showing good agreement. The estimated frequencies ...
Large eddy simulations (LES) of turbulent non-premixed swirling flames based on the Sydney swirl bur...
Large-Eddy Simulation (LES) has become a potent tool to investigate instabilities in swirl flows eve...
This study deals with the fundamental problem of combustion dynamics in gas turbine combustors op- e...
International audienceThe hydrodynamic instability in an industrial, two-staged, counter-rotative, s...
Shape optimization with respect to the suppression or enhancement of dynamical flow structures is an...
The large-scale coherent motions in a realistic swirl fuel-injector geometry are analysed by direct ...
The large-scale coherent motions in a realistic swirl fuel injector geometry are analysed by direct ...
AbstractSelf-excited helical flow oscillations are frequently observed in gas turbine combustors. In...
Hydrodynamic oscillations in gas turbine fuel injectors help to mix the fuel and air but can also co...
Hydrodynamic instabilities in gas turbine fuel injectors help to mix the fuel and air but can someti...
[EN] The main challenge of next-generation aeronautical gas turbine engines lies in the increase of ...
This thesis deals with the physics of turbulent swirling flows. Large eddy simulation (LES) method i...
International audienceDespite being good candidates for the reduction of pollutant emissions from ga...
This paper concerns the study of high Reynolds and high swirl number flow through the use of PIV mea...
International audienceWe study the liquid flow inside a recessed gas-centered swirl coaxial injector...
Large eddy simulations (LES) of turbulent non-premixed swirling flames based on the Sydney swirl bur...
Large-Eddy Simulation (LES) has become a potent tool to investigate instabilities in swirl flows eve...
This study deals with the fundamental problem of combustion dynamics in gas turbine combustors op- e...
International audienceThe hydrodynamic instability in an industrial, two-staged, counter-rotative, s...
Shape optimization with respect to the suppression or enhancement of dynamical flow structures is an...
The large-scale coherent motions in a realistic swirl fuel-injector geometry are analysed by direct ...
The large-scale coherent motions in a realistic swirl fuel injector geometry are analysed by direct ...
AbstractSelf-excited helical flow oscillations are frequently observed in gas turbine combustors. In...
Hydrodynamic oscillations in gas turbine fuel injectors help to mix the fuel and air but can also co...
Hydrodynamic instabilities in gas turbine fuel injectors help to mix the fuel and air but can someti...
[EN] The main challenge of next-generation aeronautical gas turbine engines lies in the increase of ...
This thesis deals with the physics of turbulent swirling flows. Large eddy simulation (LES) method i...
International audienceDespite being good candidates for the reduction of pollutant emissions from ga...
This paper concerns the study of high Reynolds and high swirl number flow through the use of PIV mea...
International audienceWe study the liquid flow inside a recessed gas-centered swirl coaxial injector...
Large eddy simulations (LES) of turbulent non-premixed swirling flames based on the Sydney swirl bur...
Large-Eddy Simulation (LES) has become a potent tool to investigate instabilities in swirl flows eve...
This study deals with the fundamental problem of combustion dynamics in gas turbine combustors op- e...