The aim of this work is to gain an insight on the effect of the wall heating on the aeroacoustic sound radiated by bluff bodies in laminar flows. In particular, the local thermal treatment of the wall boundary was investigated as a possible method for active controlling the emitted noise. This technique was studied performing direct numerical simulations of the aeroacoustic noise produced by an isolated square cylinder operating at a Reynolds and Mach numbers equal to 150 and 0.2, respectively. In the considered case, the Karman vortex street deriving by the flow/cylinder interaction, produces a lift and drag pulsation on the body surface, leading to a dipolar-like noise emission. In this context, different local thermal fluxes were applied...
This paper presents the results of an experimental investigation of the sound produced by flow inter...
The effect of placing a wedge in the wake of a square cylinder (side length D) at a Reynolds number ...
Aeroacoustic predictions of a model airframe noise problem are conducted in order to assess the effe...
The aim of this work is to gain an insight on the effect of the wall heating on the aeroacoustic sou...
This work presents results of a direct computation of acoustic fields produced by several laminar fl...
Aeroengine noise is one of the dominating noise sources in today’s aircraft. Reduction of the aeroen...
Community noise is one of the most poorly controlled environmental pollutants. Controlling the noise...
The present work focuses on the study of noise generation and radiation of unsteady laminar flow ove...
Laminar vortex sheddings behind a circular cylinder with and without splitter plates attached to the...
Flows past a hemisphere and their noise generation are investigated at the Reynolds numbers (Re) of ...
array, azimuthal decomposition technique (ADT), large eddy simulation (LES). Abstract Well-known sit...
The present work focuses on the study of noise generation and radiation of an infinite open three-di...
The generation of aeolian tones from a two-dimensional circular cylinder situated in a uniform cross...
Analytical solutions for the problem of radiation of sound from a duct with flow have been shown to ...
The case of a rigid flat plate placed in the wake of a square cylinder for passive sound control is ...
This paper presents the results of an experimental investigation of the sound produced by flow inter...
The effect of placing a wedge in the wake of a square cylinder (side length D) at a Reynolds number ...
Aeroacoustic predictions of a model airframe noise problem are conducted in order to assess the effe...
The aim of this work is to gain an insight on the effect of the wall heating on the aeroacoustic sou...
This work presents results of a direct computation of acoustic fields produced by several laminar fl...
Aeroengine noise is one of the dominating noise sources in today’s aircraft. Reduction of the aeroen...
Community noise is one of the most poorly controlled environmental pollutants. Controlling the noise...
The present work focuses on the study of noise generation and radiation of unsteady laminar flow ove...
Laminar vortex sheddings behind a circular cylinder with and without splitter plates attached to the...
Flows past a hemisphere and their noise generation are investigated at the Reynolds numbers (Re) of ...
array, azimuthal decomposition technique (ADT), large eddy simulation (LES). Abstract Well-known sit...
The present work focuses on the study of noise generation and radiation of an infinite open three-di...
The generation of aeolian tones from a two-dimensional circular cylinder situated in a uniform cross...
Analytical solutions for the problem of radiation of sound from a duct with flow have been shown to ...
The case of a rigid flat plate placed in the wake of a square cylinder for passive sound control is ...
This paper presents the results of an experimental investigation of the sound produced by flow inter...
The effect of placing a wedge in the wake of a square cylinder (side length D) at a Reynolds number ...
Aeroacoustic predictions of a model airframe noise problem are conducted in order to assess the effe...