Direct numerical simulation of a confined laminar premixed flame has been performed in an anechoic combustor, showing self-sustained intrinsic thermoacoustic oscillations. Theoretical predictions based on acoustic jump relations and the n − τ model for the flame are presented and causality concerns are discussed. The instability’s frequency and mode structure are recovered numerically with very good accuracy. A detailed discussion on the interplay of the physical phenomena responsible for this dynamical coupling is also carried out
Turbulent-flow interactions with the outlet guide vanes are known to mainly contribute to broadband-...
With stratospheric flight ormartian exploration in perspective, the compressibility influence on the...
The streamwise breathing motion of the separation bubble, triggered by the shock wave/boundary layer...
International audienceDirect numerical simulation of a confined laminar premixed flame has been perf...
Combustion instabilities can develop in modern gas-turbines as large amplitude pressure oscillations...
Large power densities in gas turbines can be accompanied by combustion instabilities (Culick & Kuent...
An Uncertainty Quantification (UQ) method based on active subspace and low-order models is applied o...
Monte Carlo and Active Subspace Identification methods are combined with first- and second-order adj...
A Large Eddy Simulation of a subsonic operating point (test case number two from Bake et al. [9]) of...
This paper describes the application of a coupled Acoustic model/LES approach to assess the effect o...
T-junctions correspond to a classical academic configuration employed to unravel the vortexsound int...
Since its introduction in the late 19th century, symmetry breaking has been found to play a crucial ...
This work proposes an improvement to existing methods based on modal expansions used for the predict...
International audienceThe secondary flow generated by the clearance between an isolated airfoil tip ...
International audienceThe noise produced by rotating systems such as fans and turbo machines is of g...
Turbulent-flow interactions with the outlet guide vanes are known to mainly contribute to broadband-...
With stratospheric flight ormartian exploration in perspective, the compressibility influence on the...
The streamwise breathing motion of the separation bubble, triggered by the shock wave/boundary layer...
International audienceDirect numerical simulation of a confined laminar premixed flame has been perf...
Combustion instabilities can develop in modern gas-turbines as large amplitude pressure oscillations...
Large power densities in gas turbines can be accompanied by combustion instabilities (Culick & Kuent...
An Uncertainty Quantification (UQ) method based on active subspace and low-order models is applied o...
Monte Carlo and Active Subspace Identification methods are combined with first- and second-order adj...
A Large Eddy Simulation of a subsonic operating point (test case number two from Bake et al. [9]) of...
This paper describes the application of a coupled Acoustic model/LES approach to assess the effect o...
T-junctions correspond to a classical academic configuration employed to unravel the vortexsound int...
Since its introduction in the late 19th century, symmetry breaking has been found to play a crucial ...
This work proposes an improvement to existing methods based on modal expansions used for the predict...
International audienceThe secondary flow generated by the clearance between an isolated airfoil tip ...
International audienceThe noise produced by rotating systems such as fans and turbo machines is of g...
Turbulent-flow interactions with the outlet guide vanes are known to mainly contribute to broadband-...
With stratospheric flight ormartian exploration in perspective, the compressibility influence on the...
The streamwise breathing motion of the separation bubble, triggered by the shock wave/boundary layer...