A turbulent round jet at the Reynolds number of 7,290 is simulated by direct numerical simulation to study jet noise source and its propagation. A large domain of 60 diameters in the axial direction, 30 diameters in the radial direction, and full 360 degrees is chosen to minimize the effect of boundary conditions. The spatial statistics of the simulated flow and the peak amplitude of acoustic radiation at 45-degree angle agree well with existing literature, confirming the quality of the data. Motivated by the Ffowcs-Williams and Hawkings equation, acoustic spectra at three representative locations of the potential core, the shear layer, and the ambient indicate that the fluctuation magnitudes are highest in the shear layer, followed by the ...
International audienceTwo temporally developing isothermal round jets at a Mach number of 0.9 and Re...
Jet noise is one of the major noise sources of jet-powered aircraft. To improve the understanding of...
This thesis deals with the computation and the investigation of the noise radiated by a rocket-like ...
Noise standards around the world for aircrafts have become more stringent. Jet noise is a major sour...
... jet are investigated by direct numerical simulation. Details of the numerical method are briefly...
Jet noise is an extensively studied phenomenon since the deployment of the first civil jet aircraft ...
In this work, we propose a cost-effective approach allowing one to evaluate the acoustic field gener...
International audienceIn this work,we propose a cost-effective approach allowing one to evaluate the...
Jet noise is a major concern in the design of commercial aircraft. Studies by various researchers su...
In this paper we present the experimental results of a detailed investigation of the flow and acoust...
Large Eddy Simulation (LES) is an efficient computational approach to study turbulent flows and has ...
Strict noise regulations at major airports and increasing environmental concerns have made predictio...
Direct numerical simulations of turbulent flows and their radiated acoustic fields offer a detailed ...
The ability to predict jet noise is crucial for the aviation industry, particularly in order to meet...
This study falls within the field of aircraft noise reduction and more precisely jet noise as it rep...
International audienceTwo temporally developing isothermal round jets at a Mach number of 0.9 and Re...
Jet noise is one of the major noise sources of jet-powered aircraft. To improve the understanding of...
This thesis deals with the computation and the investigation of the noise radiated by a rocket-like ...
Noise standards around the world for aircrafts have become more stringent. Jet noise is a major sour...
... jet are investigated by direct numerical simulation. Details of the numerical method are briefly...
Jet noise is an extensively studied phenomenon since the deployment of the first civil jet aircraft ...
In this work, we propose a cost-effective approach allowing one to evaluate the acoustic field gener...
International audienceIn this work,we propose a cost-effective approach allowing one to evaluate the...
Jet noise is a major concern in the design of commercial aircraft. Studies by various researchers su...
In this paper we present the experimental results of a detailed investigation of the flow and acoust...
Large Eddy Simulation (LES) is an efficient computational approach to study turbulent flows and has ...
Strict noise regulations at major airports and increasing environmental concerns have made predictio...
Direct numerical simulations of turbulent flows and their radiated acoustic fields offer a detailed ...
The ability to predict jet noise is crucial for the aviation industry, particularly in order to meet...
This study falls within the field of aircraft noise reduction and more precisely jet noise as it rep...
International audienceTwo temporally developing isothermal round jets at a Mach number of 0.9 and Re...
Jet noise is one of the major noise sources of jet-powered aircraft. To improve the understanding of...
This thesis deals with the computation and the investigation of the noise radiated by a rocket-like ...