The idea of using mixing enhancement to reduce jet noise is not new. Lobed mixers have been around since shortly after jet noise became a problem. However, these designs were often a post-design fix that rarely was worth its weight and thrust loss from a system perspective. Recent advances in CFD and some inspired concepts involving chevrons have shown how mixing enhancement can be successfully employed in noise reduction by subtle manipulation of the nozzle geometry. At NASA Glenn Research Center, this recent success has provided an opportunity to explore our paradigms of jet noise understanding, prediction, and reduction. Recent advances in turbulence measurement technology for hot jets have also greatly aided our ability to explore the c...
With the emergence of more powerful fighter aircraft, supersonic jet noise reduction devices are bei...
This paper presents diagnostic experiments aimed at understanding and mitigating supersonic jet nois...
The goal of the current research work is to develop a stand-alone jet noise prediction methodology. ...
Comparison of turbulence data taken in three separate flow nozzles, two with mixing enhancement feat...
A mixing layer is a common model used to study the noise generation and mixing characteristics of th...
High speed exhaust noise reduction continues to be a research challenge for supersonic cruise busine...
Typical installed separate-flow exhaust nozzle system. The jet noise from modern turbofan engines is...
We report on an experimental and reduced-order modeling study aimed at reducing mixing noise in hot ...
Aircraft noise mitigation is an ongoing challenge for the aeronautics research community. In respons...
This paper presents the effects of several mixing enhancement devices on turbulence in jet nozzles. ...
The source noise portion of the High Speed Research Program at NASA LeRC is focused on jet noise red...
The NASA Glenn Research Center recently completed an experimental study to reduce the jet noise from...
Fundamental mechanisms of jet noise are investigated by means of direct numerical simulation. In the...
Abstract: Jet noise remains a significant aircraft noise contributor, and for modern high-bypass-rat...
The notched nozzle as a new concept has been investigated for conventional nozzle design together wi...
With the emergence of more powerful fighter aircraft, supersonic jet noise reduction devices are bei...
This paper presents diagnostic experiments aimed at understanding and mitigating supersonic jet nois...
The goal of the current research work is to develop a stand-alone jet noise prediction methodology. ...
Comparison of turbulence data taken in three separate flow nozzles, two with mixing enhancement feat...
A mixing layer is a common model used to study the noise generation and mixing characteristics of th...
High speed exhaust noise reduction continues to be a research challenge for supersonic cruise busine...
Typical installed separate-flow exhaust nozzle system. The jet noise from modern turbofan engines is...
We report on an experimental and reduced-order modeling study aimed at reducing mixing noise in hot ...
Aircraft noise mitigation is an ongoing challenge for the aeronautics research community. In respons...
This paper presents the effects of several mixing enhancement devices on turbulence in jet nozzles. ...
The source noise portion of the High Speed Research Program at NASA LeRC is focused on jet noise red...
The NASA Glenn Research Center recently completed an experimental study to reduce the jet noise from...
Fundamental mechanisms of jet noise are investigated by means of direct numerical simulation. In the...
Abstract: Jet noise remains a significant aircraft noise contributor, and for modern high-bypass-rat...
The notched nozzle as a new concept has been investigated for conventional nozzle design together wi...
With the emergence of more powerful fighter aircraft, supersonic jet noise reduction devices are bei...
This paper presents diagnostic experiments aimed at understanding and mitigating supersonic jet nois...
The goal of the current research work is to develop a stand-alone jet noise prediction methodology. ...