Closed-Circuit wind tunnels in which air is driven by fans are widely used for aerodynamic testing. For aeroacoustic tests, in which the radiated sound field must be measured in the presence of flow, they have two major problems: the fan makes them noisy, and the hard walls make them reverberant. The ideal aeroacoustic test facility would be quiet and anechoic. It is difficult to satisfy these requirements in a standard wind tunnel because anechoic and noise-muffling treatments tend to increase flow resistance so that the fan has to work harder resulting in more noise. In this Note a novel alternative that will eliminate the fan and allow as much anechoic treatment as desired will be proposed
This paper presents the design and performance of an open jet, blow down wind tunnel that was newly ...
The increasing attention given to aerodynamically generated noise brings into focus the need for qua...
The anechoic open-jet wind tunnel facility at the University of Toronto Institute for Aerospace Stud...
ABSTRACT: This paper describes the update and characterization of a previously pure aerodynamics win...
The anechoic chamber of "hepia - Genève" was modified with the purpouse to host a removable wind tun...
The noise (unwanted sound) from fans of all sizes, operating in close proximity to people, can be a ...
This paper describes the UTwente Aeroacoustic Wind Tunnel including its recent anechoic chamber reno...
The development of fan noise reduction measures that specifically address the sources requires detai...
Measures to reduce the intensity of fan noise in the NASA Langley 30 ft x 60 ft subsonic wind tunnel...
The phased microphone array has become a widely used tool in aeroacoustic testing for the localisati...
August 1972Includes bibliographical references (leaf 12)An open-jet wind tunnel operating within an ...
A small didactic wind tunnel demonstrator has been designed and manufactured at the von Karman Insti...
Semi-buried engines are part of of many future aircraft designs. From acoustic’s point of view the i...
This paper presents the design and performance of an open jet, blow down wind tunnel that was newly ...
Acoustic imaging is an indispensable experimental aid in the design of silent aircraft. In this work...
This paper presents the design and performance of an open jet, blow down wind tunnel that was newly ...
The increasing attention given to aerodynamically generated noise brings into focus the need for qua...
The anechoic open-jet wind tunnel facility at the University of Toronto Institute for Aerospace Stud...
ABSTRACT: This paper describes the update and characterization of a previously pure aerodynamics win...
The anechoic chamber of "hepia - Genève" was modified with the purpouse to host a removable wind tun...
The noise (unwanted sound) from fans of all sizes, operating in close proximity to people, can be a ...
This paper describes the UTwente Aeroacoustic Wind Tunnel including its recent anechoic chamber reno...
The development of fan noise reduction measures that specifically address the sources requires detai...
Measures to reduce the intensity of fan noise in the NASA Langley 30 ft x 60 ft subsonic wind tunnel...
The phased microphone array has become a widely used tool in aeroacoustic testing for the localisati...
August 1972Includes bibliographical references (leaf 12)An open-jet wind tunnel operating within an ...
A small didactic wind tunnel demonstrator has been designed and manufactured at the von Karman Insti...
Semi-buried engines are part of of many future aircraft designs. From acoustic’s point of view the i...
This paper presents the design and performance of an open jet, blow down wind tunnel that was newly ...
Acoustic imaging is an indispensable experimental aid in the design of silent aircraft. In this work...
This paper presents the design and performance of an open jet, blow down wind tunnel that was newly ...
The increasing attention given to aerodynamically generated noise brings into focus the need for qua...
The anechoic open-jet wind tunnel facility at the University of Toronto Institute for Aerospace Stud...