Experimental investigation of flow-induced sound and sources of sound necessitates an adequate environment of low interfering noise and suppression of unwanted sources of sound. In order to investigate the sound from fluid-structure interactions, a low-noise wind tunnel has been designed and implemented. This paper gives an overview of the design criteria and specifications, along with an aeroacoustic and aerodynamic characterization of the facility. The suitability to airfoil self-noise studies is explored and first measurements with a model airfoil are presented. The paper concludes with suggestions for improvements and provides an outlook on future applications. CONCEPT AND DESIGN OF THE WIND TUNNE
This paper describes an experimental investigation of the interaction noise in a jet impacting isola...
This thesis describes an investigation into the aeroacoustic noise produced by an aerofoil using ex...
The experimental technique of aeroacoustic imaging is critical to validate the low noise design meth...
This paper presents the design and performance of an open jet, blow down wind tunnel that was newly ...
This paper presents the design and performance of an open jet, blow down wind tunnel that was newly ...
A small anechoic wind tunnel was built at the University of Adelaide, School of Mechanical Engineeri...
An experimental investigation into airfoil self-noise (trailing edge noise, tip vortex formation noi...
August 1972Includes bibliographical references (leaf 12)An open-jet wind tunnel operating within an ...
This experimental works summarize the (1), aeroacoustic results of airfoil self-noise generated at R...
A small didactic wind tunnel demonstrator has been designed and manufactured at the von Karman Insti...
A small didactic wind tunnel demonstrator has been designed and manufactured at the von Karman Insti...
A small didactic wind tunnel demonstrator has been designed and manufactured at the von Karman Insti...
microphone array, windturbine noise, trailing edge noise, inflow-turbulence noise Aeroacoustic wind ...
Paper Number 47In order to produce aircraft, turbo-machinery and helicopters with low acoustic signa...
Aerodynamically generated noise affects passenger comfort in cars, high-speed trains, and airplanes,...
This paper describes an experimental investigation of the interaction noise in a jet impacting isola...
This thesis describes an investigation into the aeroacoustic noise produced by an aerofoil using ex...
The experimental technique of aeroacoustic imaging is critical to validate the low noise design meth...
This paper presents the design and performance of an open jet, blow down wind tunnel that was newly ...
This paper presents the design and performance of an open jet, blow down wind tunnel that was newly ...
A small anechoic wind tunnel was built at the University of Adelaide, School of Mechanical Engineeri...
An experimental investigation into airfoil self-noise (trailing edge noise, tip vortex formation noi...
August 1972Includes bibliographical references (leaf 12)An open-jet wind tunnel operating within an ...
This experimental works summarize the (1), aeroacoustic results of airfoil self-noise generated at R...
A small didactic wind tunnel demonstrator has been designed and manufactured at the von Karman Insti...
A small didactic wind tunnel demonstrator has been designed and manufactured at the von Karman Insti...
A small didactic wind tunnel demonstrator has been designed and manufactured at the von Karman Insti...
microphone array, windturbine noise, trailing edge noise, inflow-turbulence noise Aeroacoustic wind ...
Paper Number 47In order to produce aircraft, turbo-machinery and helicopters with low acoustic signa...
Aerodynamically generated noise affects passenger comfort in cars, high-speed trains, and airplanes,...
This paper describes an experimental investigation of the interaction noise in a jet impacting isola...
This thesis describes an investigation into the aeroacoustic noise produced by an aerofoil using ex...
The experimental technique of aeroacoustic imaging is critical to validate the low noise design meth...