In an attempt to determine the parameters characterizing the noise environment in transonic tunnels, noise-generating mechanisms for porous-wall tunnels with 60-deg inclined holes were isolated and studied. The noise environment in the test section is separated into three distinct parts: the noise due to jet flow through the porous walls, a wall hole-tunnel resonance phenomena, and the turbulent boundary layer on the test section walls and in the diffuser. Each part is analyzed separately for the effects of aerodynamic and geometric flow constraints on the frequency and power characteristics. The contribution of each of the acoustic models to the test section free-stream fluctuating pressure level is also examined.Report was prepared by ARO...
A study was conducted to investigate the effects of wind tunnel test section noise on the location o...
Background noise measurements were made of the acoustic environment in the National Full-Scale Aerod...
The equivalent porosity of the test section wall in a transonic wind tunnel with a fixed geometric p...
The report presents the results of recent studies of noise in Propulsion Wind Tunnel (16T) and Aerod...
An experimental investigation of acoustic disturbances and means of suppression from ventilated tran...
This study focuses on the acoustic installation effects that may occur during typical aeroacoustic e...
The noise level of wind tunnel test section is respected as one of the most important performance sp...
An experimental investigation was conducted to determine the effects of radiated aerodynamic-noise o...
August 1972Includes bibliographical references (leaf 12)An open-jet wind tunnel operating within an ...
The modern trend towards high engine power and large13; aeronautical test facilities has resulted in...
Aerodynamic noise produced by aircraft, wind turbines, and other objects subjected to airflow contri...
A study of the impact of reverberation on cruise regime acoustic testing of contra-rotating open rot...
The motivation of the performed investigations lies in the fact, that flow noises occur at façade el...
The measurement of wind tunnel background pressure fluctuations in a Ludwig Tube is discussed. The m...
When a turbulent boundary layer is produced by air flow past a. solid surface, the turbulence in the...
A study was conducted to investigate the effects of wind tunnel test section noise on the location o...
Background noise measurements were made of the acoustic environment in the National Full-Scale Aerod...
The equivalent porosity of the test section wall in a transonic wind tunnel with a fixed geometric p...
The report presents the results of recent studies of noise in Propulsion Wind Tunnel (16T) and Aerod...
An experimental investigation of acoustic disturbances and means of suppression from ventilated tran...
This study focuses on the acoustic installation effects that may occur during typical aeroacoustic e...
The noise level of wind tunnel test section is respected as one of the most important performance sp...
An experimental investigation was conducted to determine the effects of radiated aerodynamic-noise o...
August 1972Includes bibliographical references (leaf 12)An open-jet wind tunnel operating within an ...
The modern trend towards high engine power and large13; aeronautical test facilities has resulted in...
Aerodynamic noise produced by aircraft, wind turbines, and other objects subjected to airflow contri...
A study of the impact of reverberation on cruise regime acoustic testing of contra-rotating open rot...
The motivation of the performed investigations lies in the fact, that flow noises occur at façade el...
The measurement of wind tunnel background pressure fluctuations in a Ludwig Tube is discussed. The m...
When a turbulent boundary layer is produced by air flow past a. solid surface, the turbulence in the...
A study was conducted to investigate the effects of wind tunnel test section noise on the location o...
Background noise measurements were made of the acoustic environment in the National Full-Scale Aerod...
The equivalent porosity of the test section wall in a transonic wind tunnel with a fixed geometric p...