Linearized Euler equations are used to simulate supersonic jet noise generation and propagation. Special attention is given to boundary treatment. The resulting solution is stable and nearly free from boundary reflections without the need for artificial dissipation, filtering, or a sponge layer. The computed solution is in good agreement with theory and observation and is much less CPU-intensive as compared to large-eddy simulations
The problem of intense sound radiation from supersonic jets is a concern for both civil and military...
Development of concepts for reduction of jet noise has relied heavily on expensive experimental test...
This paper presents stability calculations made for a shock-free supersonic jet using the model base...
An improved version of a previously validated linearized Euler equation solver is used to compute th...
An efficient method for calculating linearized disturbances to shear flows that accurately captures ...
Accurate prediction of jet fan and exhaust plume flow and noise generation and propagation is very i...
A rather novel approach to predict jet noise is the Stochastic Noise Generation and Radiation (SNGR)...
Experimental and numerical investigations have correlated large-scale coherent structures in turbule...
An approximate technique is presented for the prediction of the large-scale turbulent structure soun...
Jet noise is directly predicted using large-scale equations. The computational domain is extended in...
Some numerical solutions of acoustic propagation problems using linearized Euler equations are studi...
The computations of axisymmetric jet noise with symmetric disturbances are investigated using the di...
Larger aircraft with new high performance engines in combination with cities growing closer to urban...
An acoustic analogy is developed to predict the noise from jet flows. It contains two source models ...
We present a new method for stability and modal analysis of shear flows and their acoustic radiation...
The problem of intense sound radiation from supersonic jets is a concern for both civil and military...
Development of concepts for reduction of jet noise has relied heavily on expensive experimental test...
This paper presents stability calculations made for a shock-free supersonic jet using the model base...
An improved version of a previously validated linearized Euler equation solver is used to compute th...
An efficient method for calculating linearized disturbances to shear flows that accurately captures ...
Accurate prediction of jet fan and exhaust plume flow and noise generation and propagation is very i...
A rather novel approach to predict jet noise is the Stochastic Noise Generation and Radiation (SNGR)...
Experimental and numerical investigations have correlated large-scale coherent structures in turbule...
An approximate technique is presented for the prediction of the large-scale turbulent structure soun...
Jet noise is directly predicted using large-scale equations. The computational domain is extended in...
Some numerical solutions of acoustic propagation problems using linearized Euler equations are studi...
The computations of axisymmetric jet noise with symmetric disturbances are investigated using the di...
Larger aircraft with new high performance engines in combination with cities growing closer to urban...
An acoustic analogy is developed to predict the noise from jet flows. It contains two source models ...
We present a new method for stability and modal analysis of shear flows and their acoustic radiation...
The problem of intense sound radiation from supersonic jets is a concern for both civil and military...
Development of concepts for reduction of jet noise has relied heavily on expensive experimental test...
This paper presents stability calculations made for a shock-free supersonic jet using the model base...