computed by a compressible Large Eddy Simulation (LES) to determine both the flow field and the sound field in the same calculation. The noise radiated by the jet, provided by LES, is in good agreement with experimental data of the literature in terms of sound pressure spectra, levels and directivity, showing the feasibility of this direct noise calculation. The dominant sound generation mechanism is also investigated, by presenting a correlation between its radiation, observed for an angle of 30 ◦ from the downstream direction, and the intrusion of vortical structures into the jet core. To cite this article: C. Bogey
Flow and noise solutions using Large Eddy Simulation (LES) are evaluated for two jets at acoustic Ma...
Large-Eddy Simulations (LES) of a compressible nozzle/jet configuration have been carried out. Two j...
In this paper, the data obtained by LES for an initially laminar and overexpanded jet at Mach number...
Noise sources are investigated in subsonic jets at Mach numbers M = 0.6 and M = 0.9, with Reynolds n...
Computational simulation techniques produce considerably more information about turbulent jets than ...
The source of the jet noise is generated by rocket exhaust plume during rocket engine testing. A dom...
from 1.7×103 to 4×105 are investigated using Large Eddy Simulations. As the Reynolds number decrease...
Jet noise is an extensively studied phenomenon since the deployment of the first civil jet aircraft ...
Increasing noise regulations at urban airports force jet engine manufactures to develop and build mo...
The calculation of noise generated by a jet of viscous compressible gas flowing out from a conical n...
In this paper numerical simulations are used to calculate the turbulence dynamics simultaneously wit...
AbstractExperiment and direct numerical simulation provide compelling evidence that nonlinear wave i...
Large Eddy Simulation (LES) is an efficient computational approach to study turbulent flows and has ...
Large eddy simulations (LES) of a subsonic plane jet at a Mach number of 0.9 and a Reynolds number o...
Large-Eddy Simulations (LES) of a compressible nozzle/jet configuration have been carried out. Two j...
Flow and noise solutions using Large Eddy Simulation (LES) are evaluated for two jets at acoustic Ma...
Large-Eddy Simulations (LES) of a compressible nozzle/jet configuration have been carried out. Two j...
In this paper, the data obtained by LES for an initially laminar and overexpanded jet at Mach number...
Noise sources are investigated in subsonic jets at Mach numbers M = 0.6 and M = 0.9, with Reynolds n...
Computational simulation techniques produce considerably more information about turbulent jets than ...
The source of the jet noise is generated by rocket exhaust plume during rocket engine testing. A dom...
from 1.7×103 to 4×105 are investigated using Large Eddy Simulations. As the Reynolds number decrease...
Jet noise is an extensively studied phenomenon since the deployment of the first civil jet aircraft ...
Increasing noise regulations at urban airports force jet engine manufactures to develop and build mo...
The calculation of noise generated by a jet of viscous compressible gas flowing out from a conical n...
In this paper numerical simulations are used to calculate the turbulence dynamics simultaneously wit...
AbstractExperiment and direct numerical simulation provide compelling evidence that nonlinear wave i...
Large Eddy Simulation (LES) is an efficient computational approach to study turbulent flows and has ...
Large eddy simulations (LES) of a subsonic plane jet at a Mach number of 0.9 and a Reynolds number o...
Large-Eddy Simulations (LES) of a compressible nozzle/jet configuration have been carried out. Two j...
Flow and noise solutions using Large Eddy Simulation (LES) are evaluated for two jets at acoustic Ma...
Large-Eddy Simulations (LES) of a compressible nozzle/jet configuration have been carried out. Two j...
In this paper, the data obtained by LES for an initially laminar and overexpanded jet at Mach number...