In the current jet noise study, an empirical modal decomposition is proposed which distills the noisy and quiet modes of the flow field. In particular, the POD of flows is generalised for an optimal resolution of the far-field noise as opposed to a least-order rep-resentation of the hydrodynamic fluctuation level. This decomposition technique, which we call ‘most observable decomposition (MOD)’, is based on a linear cause-effect relationship between the hydrodynamics (cause) and the far-field acoustics (observed effect). In the current study, this relationship is identified from a linear stochastic estimation between the flow field and the far-field pressure — taking into account the propagation time of sound. We employ MOD to turbulent jet...
To calculate the noise emanating from a turbulent flow (such as a jet flow) using Lighthill's analog...
A semi-empirical far-field jet noise acoustic model derived using the energy spectrum function is pr...
Large Eddy Simulation (LES) is an efficient computational approach to study turbulent flows and has ...
In the present study, subsonic turbulent jet noise is investigated employing reduced-order represen...
We analyze the far field acoustic power spectrum of a jet flow convecting a region of turbulent acti...
Resolvent analysis continues to provide promising results for modeling the hydrodynamic near-field a...
In this work an experimental investigation of the near-field pressure of a compressible jet is prese...
A reduced-ordermodelling (ROM) strategy is pursued to achieve a mechanistic understanding of jet flo...
This paper examines some recent, developments in the modeling of supersonic jet noise using a com-pr...
A Proper Orthogonal Decomposition (POD) is constructed for a Mach 0.9 turbulent jet using a well-va...
Supersonic jet noise has been an important research topic for decades, both for its relevance within...
The most energetic modes of the turbulent mixing layer from an axisymmetric jet at Mach 0.85 are exa...
This paper details the statistical and time-resolved analysis of the relationship between the near-f...
The goal of this effort has been to identify the dominant source of the radiated aero-acoustic noise...
Choked operation of model jets with unheated air indicates the appearence of a discrete-frequency co...
To calculate the noise emanating from a turbulent flow (such as a jet flow) using Lighthill's analog...
A semi-empirical far-field jet noise acoustic model derived using the energy spectrum function is pr...
Large Eddy Simulation (LES) is an efficient computational approach to study turbulent flows and has ...
In the present study, subsonic turbulent jet noise is investigated employing reduced-order represen...
We analyze the far field acoustic power spectrum of a jet flow convecting a region of turbulent acti...
Resolvent analysis continues to provide promising results for modeling the hydrodynamic near-field a...
In this work an experimental investigation of the near-field pressure of a compressible jet is prese...
A reduced-ordermodelling (ROM) strategy is pursued to achieve a mechanistic understanding of jet flo...
This paper examines some recent, developments in the modeling of supersonic jet noise using a com-pr...
A Proper Orthogonal Decomposition (POD) is constructed for a Mach 0.9 turbulent jet using a well-va...
Supersonic jet noise has been an important research topic for decades, both for its relevance within...
The most energetic modes of the turbulent mixing layer from an axisymmetric jet at Mach 0.85 are exa...
This paper details the statistical and time-resolved analysis of the relationship between the near-f...
The goal of this effort has been to identify the dominant source of the radiated aero-acoustic noise...
Choked operation of model jets with unheated air indicates the appearence of a discrete-frequency co...
To calculate the noise emanating from a turbulent flow (such as a jet flow) using Lighthill's analog...
A semi-empirical far-field jet noise acoustic model derived using the energy spectrum function is pr...
Large Eddy Simulation (LES) is an efficient computational approach to study turbulent flows and has ...