International audienceFour initially highly-disturbed overexpanded round jets at an exit Mach number of 3.1 and a Reynolds number of 2&_times; 10<sup>5</sup> have been computed by Large-Eddy Simulation (LES). The static pressure and temperature at the nozzle exit are respectively equal to 0.63 &_times; 10<sup>5</sup> Pa and 738 K. One jet is free whereas the three other ones impinge on a plate located at a distance of L=30r<sub>0</sub>, where r<sub>0</sub> is the nozzle radius. Two of the plates have a hole of diameter d=2.6r<sub>0</sub> and 4r<sub>0</sub> while the last one has no hole, in order to study the effects of the hole on the jet flow and acoustic fields. For ...
International audienceThe effects of moderate Reynolds numbers on the flow and acoustic fields of in...
A large-eddy simulation (LES) of a compressible nozzle/jet configuration has been carried out. An is...
International audienceIn this study, the methodology relying on LES for the generation of the acoust...
International audienceLarge-eddy simulations (LES) of five overexpanded rocket jets impinging on a p...
International audienceFour initially highly disturbed round jets at a Mach number of 0.9 impinging o...
International audienceThe generation of acoustic tones in four round jets at a Mach number of 0.9 im...
An initially laminar overexpanded round jet at an exit Mach number of 3.30 and a Reynolds number of ...
Large-Eddy Simulations (LES) of a compressible nozzle/jet conguration have been car-ried out. Two je...
The acoustic radiation and the feedback mechanisms in jets impinging on a plate with a hole are inve...
A turbulent plane jet impinging on a slotted surface is simulated using Large Eddy Simulation LES. T...
International audienceThe Mach number dependence of the tones generated by round jets impinging on a...
International audienceThe noise emitted by an overexpanded round jet at a Mach number of 3.3 and a R...
The presence and properties of acoustic peaks near the nozzle of impinging rocket jets have been inv...
In the present paper, a numerical investigation has been carried out to classify and clarify the eff...
Round jets originating from a pipe nozzle are computed by Large-Eddy Simulations (LES) to investigat...
International audienceThe effects of moderate Reynolds numbers on the flow and acoustic fields of in...
A large-eddy simulation (LES) of a compressible nozzle/jet configuration has been carried out. An is...
International audienceIn this study, the methodology relying on LES for the generation of the acoust...
International audienceLarge-eddy simulations (LES) of five overexpanded rocket jets impinging on a p...
International audienceFour initially highly disturbed round jets at a Mach number of 0.9 impinging o...
International audienceThe generation of acoustic tones in four round jets at a Mach number of 0.9 im...
An initially laminar overexpanded round jet at an exit Mach number of 3.30 and a Reynolds number of ...
Large-Eddy Simulations (LES) of a compressible nozzle/jet conguration have been car-ried out. Two je...
The acoustic radiation and the feedback mechanisms in jets impinging on a plate with a hole are inve...
A turbulent plane jet impinging on a slotted surface is simulated using Large Eddy Simulation LES. T...
International audienceThe Mach number dependence of the tones generated by round jets impinging on a...
International audienceThe noise emitted by an overexpanded round jet at a Mach number of 3.3 and a R...
The presence and properties of acoustic peaks near the nozzle of impinging rocket jets have been inv...
In the present paper, a numerical investigation has been carried out to classify and clarify the eff...
Round jets originating from a pipe nozzle are computed by Large-Eddy Simulations (LES) to investigat...
International audienceThe effects of moderate Reynolds numbers on the flow and acoustic fields of in...
A large-eddy simulation (LES) of a compressible nozzle/jet configuration has been carried out. An is...
International audienceIn this study, the methodology relying on LES for the generation of the acoust...