The application of a synthetic jet actuator in workplaces entails the necessity of noise reduction, which they generate. One of the methods to achieve this is the use of the chevron orifice or nozzle. Therefore, the impact of different numbers of chevrons and rounding of cutouts in the orifice on the actuator efficiency and the sound pressure level was tested. The chevron orifices were compared to the circular orifice. The time-mean reaction force method was used to measured efficiency and flow parameters, and the noise was measured according to the ISO 3746:2010. The rounded cutouts had an advantageous impact on the actuator efficiency at the power P>1 W, while the efficiency of the actuator with classic chevron orifice was smaller than wi...
This is a brief summary of numerical and experimental studies, conducted between about 2003 and the ...
Aero-acoustic characteristics of a high-speed jet with chevron nozzles are experimentally investigat...
A synthetic jet is formed by periodic oscillation of a fluid through an orifice. The oscillatory mot...
With the emergence of more powerful fighter aircraft, supersonic jet noise reduction devices are bei...
The synthetic jet actuator is an active flow control device that is used to improve the aerodynamic ...
The present environmental issues have made aircraft jet noise reduction a crucial problem in aero-ac...
Experimental investigations have been carried out on beveled and asymmetric chevron nozzles to asses...
This paper describes a joint study of the acoustics of conical convergent-divergent (C-D) nozzles su...
Broadband shock noise is reduced because chevrons increase the shear-layer thickness between the fli...
This paper presents a study regarding the noise reduction of the turbojet engine, in particular the ...
The addition of chevrons to the exit of a jet has been found to reduce far-field noise, making it an...
Jet noise has been a major community concern since the 1940s. Among noise-suppression devices, chevr...
Noise from commercial high-bypass ratio turbofan engines is generated by turbulent mixing of the hot...
An axisymmetric synthetic jet actuator based on a loudspeaker and five types of flanged nozzles were...
This work details an experimental investigation aimed at reducing the noise output of piezoelectrica...
This is a brief summary of numerical and experimental studies, conducted between about 2003 and the ...
Aero-acoustic characteristics of a high-speed jet with chevron nozzles are experimentally investigat...
A synthetic jet is formed by periodic oscillation of a fluid through an orifice. The oscillatory mot...
With the emergence of more powerful fighter aircraft, supersonic jet noise reduction devices are bei...
The synthetic jet actuator is an active flow control device that is used to improve the aerodynamic ...
The present environmental issues have made aircraft jet noise reduction a crucial problem in aero-ac...
Experimental investigations have been carried out on beveled and asymmetric chevron nozzles to asses...
This paper describes a joint study of the acoustics of conical convergent-divergent (C-D) nozzles su...
Broadband shock noise is reduced because chevrons increase the shear-layer thickness between the fli...
This paper presents a study regarding the noise reduction of the turbojet engine, in particular the ...
The addition of chevrons to the exit of a jet has been found to reduce far-field noise, making it an...
Jet noise has been a major community concern since the 1940s. Among noise-suppression devices, chevr...
Noise from commercial high-bypass ratio turbofan engines is generated by turbulent mixing of the hot...
An axisymmetric synthetic jet actuator based on a loudspeaker and five types of flanged nozzles were...
This work details an experimental investigation aimed at reducing the noise output of piezoelectrica...
This is a brief summary of numerical and experimental studies, conducted between about 2003 and the ...
Aero-acoustic characteristics of a high-speed jet with chevron nozzles are experimentally investigat...
A synthetic jet is formed by periodic oscillation of a fluid through an orifice. The oscillatory mot...