Frequency dependency of the defining parameters in aero-acoustics has been a controversial issue and many theoretical and experimental studies have been directed towards its understanding and modelling. In this paper a new time scale based on the turbulent energy transfer rate is introduced and used along with the MGBK method for a short-cowl nozzle. The required CFD results for noise prediction are obtained using a modified k ? e turbulence model. Numerical results are provided for two flow working conditions, bypass velocity ratio 1 and 0.9. Besides the comparisons of the new time scale against the traditional time scale, namely dissipation time scale, corresponding noise prediction results at ninety degrees as well as other angles are co...
Current civil aircraft are significantly quieter than the civil aircraft of the 20th century. But th...
Three statistical jet noise prediction models are compared for a representative set of single-stream...
Subsonicand supersonic jet noise is determined numerically from statistical sourcemodels.The goal is...
This paper presents a study of the effects of the form of the time-scale used in aerodynamic noise p...
To calculate the noise emanating from a turbulent flow (such as a jet flow) using Lighthill's analog...
The turbulent energy dissipation rate time-scale and length-scale has been routinely used for the pr...
To calculate the noise emanating from a turbulent flow using an acoustic analogy knowledge concernin...
To calculate the noise emanating from a turbulent flow using an acoustic analogy knowledge concernin...
The acoustic analogy introduced by Lighthill to study jet noise is now over 50 years old. In the pre...
The importance of reducing jet noise in both commercial and military aircraft applications has made ...
The ability to predict jet noise is crucial for the aviation industry, particularly in order to meet...
The ability to predict jet noise is crucial for the aviation industry, particularly in order to meet...
A jet noise source model based on the Lighthill acoustic analogy is presented. Although much of the ...
ABSTRACT: The noise source distribution of a short-cowl coaxial jet operating at different velocity ...
ABSTRACT: The noise source distribution of a short-cowl coaxial jet operating at different velocity ...
Current civil aircraft are significantly quieter than the civil aircraft of the 20th century. But th...
Three statistical jet noise prediction models are compared for a representative set of single-stream...
Subsonicand supersonic jet noise is determined numerically from statistical sourcemodels.The goal is...
This paper presents a study of the effects of the form of the time-scale used in aerodynamic noise p...
To calculate the noise emanating from a turbulent flow (such as a jet flow) using Lighthill's analog...
The turbulent energy dissipation rate time-scale and length-scale has been routinely used for the pr...
To calculate the noise emanating from a turbulent flow using an acoustic analogy knowledge concernin...
To calculate the noise emanating from a turbulent flow using an acoustic analogy knowledge concernin...
The acoustic analogy introduced by Lighthill to study jet noise is now over 50 years old. In the pre...
The importance of reducing jet noise in both commercial and military aircraft applications has made ...
The ability to predict jet noise is crucial for the aviation industry, particularly in order to meet...
The ability to predict jet noise is crucial for the aviation industry, particularly in order to meet...
A jet noise source model based on the Lighthill acoustic analogy is presented. Although much of the ...
ABSTRACT: The noise source distribution of a short-cowl coaxial jet operating at different velocity ...
ABSTRACT: The noise source distribution of a short-cowl coaxial jet operating at different velocity ...
Current civil aircraft are significantly quieter than the civil aircraft of the 20th century. But th...
Three statistical jet noise prediction models are compared for a representative set of single-stream...
Subsonicand supersonic jet noise is determined numerically from statistical sourcemodels.The goal is...