Development of concepts for reduction of jet noise has relied heavily on expensive experimental testing of various nozzle designs. For example, the design of nozzle serrations (chevron) and internal mixer/ejector nozzles have relied largely on laboratory and full-scale testing. Without a deeper understanding of the sources of high-speed jet noise it is very difficult to effectively design configurations that reduce the noise and maintain other performance metrics such as nozzle thrust. In addition, the high complexity of the flow limits the success of a parametric black-box optimization
Jet noise is still a major component of overall aircraft noise emission at take-off, and its reducti...
Large eddy simulations of an isothermal Mach 0.9 jet issued from a convergent-straight nozzle are pe...
Accurate prediction of jet fan and exhaust plume flow and noise generation and propagation is very i...
Development of concepts for reduction of jet noise has relied heavily on expensive experimental test...
AbstractThe Large-Eddy Simulation (LES) numerical system established since 2002 for jet-noise comput...
This paper reviews the current state of large-eddy simulation (LES) for nozzle flows and discusses t...
Turbulent jet large-eddy simulations (LES) are performed at Mach 0.9 and Reynolds number of 106. For...
The problem of intense sound radiation from supersonic jets is a concern for both civil and military...
To improve understanding and modeling of jet-noise source mechanisms, extensive experimental and num...
To improve understanding and modeling of jet-noise source mechanisms, extensive experimental and num...
To improve understanding and modeling of jet-noise source mechanisms, extensive experimental and num...
AbstractThis paper describes a methodology for the direct calculation of noise from realistic nozzle...
In recent years, jet noise has been an active area of research due to an increase in the use of airc...
Stricter noise regulations for commercial and military aircraft have increased interest in noise red...
Jet noise is still a major component of overall aircraft noise emission at take-off, and its reducti...
Jet noise is still a major component of overall aircraft noise emission at take-off, and its reducti...
Large eddy simulations of an isothermal Mach 0.9 jet issued from a convergent-straight nozzle are pe...
Accurate prediction of jet fan and exhaust plume flow and noise generation and propagation is very i...
Development of concepts for reduction of jet noise has relied heavily on expensive experimental test...
AbstractThe Large-Eddy Simulation (LES) numerical system established since 2002 for jet-noise comput...
This paper reviews the current state of large-eddy simulation (LES) for nozzle flows and discusses t...
Turbulent jet large-eddy simulations (LES) are performed at Mach 0.9 and Reynolds number of 106. For...
The problem of intense sound radiation from supersonic jets is a concern for both civil and military...
To improve understanding and modeling of jet-noise source mechanisms, extensive experimental and num...
To improve understanding and modeling of jet-noise source mechanisms, extensive experimental and num...
To improve understanding and modeling of jet-noise source mechanisms, extensive experimental and num...
AbstractThis paper describes a methodology for the direct calculation of noise from realistic nozzle...
In recent years, jet noise has been an active area of research due to an increase in the use of airc...
Stricter noise regulations for commercial and military aircraft have increased interest in noise red...
Jet noise is still a major component of overall aircraft noise emission at take-off, and its reducti...
Jet noise is still a major component of overall aircraft noise emission at take-off, and its reducti...
Large eddy simulations of an isothermal Mach 0.9 jet issued from a convergent-straight nozzle are pe...
Accurate prediction of jet fan and exhaust plume flow and noise generation and propagation is very i...