A RANS-based numerical technique for the prediction of the airfoil trailing-edge broadband noise is presented. The definition of the sound sources from RANS turbulence statistics is based on a stochastic reconstruction of the turbulent velocity fluctuations. The method, named Eulerian Solenoidal Digital Filter, accounts for the convective transport and for the solenoidality of the velocity field. The acoustic near field is computed solving the Acoustic Perturbation Equations in the frequency domain. The integral formulation of Ffowcs Williams and Hawkings is used to evaluate the far-field radiation. The ESDF method is validated for the case of homogeneous isotropic turbulence and it is applied to the calculation of the broadband trailing...
AbstractThe current status of a hybrid RANS/CAA approach for the simulation of broadband sound gener...
The long term objective of this project is to develop a computational method for predicting the nois...
An efficient stochastic method is applied to the problem of modelling unsteady turbulent velocity fl...
A RANS-based numerical technique for the prediction of the airfoil trailing-edge broadband noise is ...
In this work a hybrid RANS/CAA methodology is used to predict trailing-edge noise of a controlled-di...
A Computational Aeroacoustic (CAA) study is conducted for the simulation of broad- band trailing-ed...
A numerical approach to predict broadband trailing-edge noise for low Mach number flows is presented...
The prediction quality of a fast Computational Aeroacoustics (CAA) approach is studied for noise gen...
In this study, a Computational Aeroacoustics (CAA) method is presented for the prediction of trailin...
Airfoil self noise is produced when an airfoil is immersed in an undisturbed flow. Flow turbulence c...
Trailing edge noise generated by turbulent flow traveling past an edge of an airfoil is one of the m...
AbstractThe current status of a hybrid RANS/CAA approach for the simulation of broadband sound gener...
A new analytic result in acoustics called 'Formulation 1B,' proposed by Farassat, is used to compute...
Trailing edge noise is simulated based on acoustic perturbation equations and a stochastic model for...
The TE noise radiated by aNACA0012 airfoil, at zero incidence, is studied. The mean turbulent flow p...
AbstractThe current status of a hybrid RANS/CAA approach for the simulation of broadband sound gener...
The long term objective of this project is to develop a computational method for predicting the nois...
An efficient stochastic method is applied to the problem of modelling unsteady turbulent velocity fl...
A RANS-based numerical technique for the prediction of the airfoil trailing-edge broadband noise is ...
In this work a hybrid RANS/CAA methodology is used to predict trailing-edge noise of a controlled-di...
A Computational Aeroacoustic (CAA) study is conducted for the simulation of broad- band trailing-ed...
A numerical approach to predict broadband trailing-edge noise for low Mach number flows is presented...
The prediction quality of a fast Computational Aeroacoustics (CAA) approach is studied for noise gen...
In this study, a Computational Aeroacoustics (CAA) method is presented for the prediction of trailin...
Airfoil self noise is produced when an airfoil is immersed in an undisturbed flow. Flow turbulence c...
Trailing edge noise generated by turbulent flow traveling past an edge of an airfoil is one of the m...
AbstractThe current status of a hybrid RANS/CAA approach for the simulation of broadband sound gener...
A new analytic result in acoustics called 'Formulation 1B,' proposed by Farassat, is used to compute...
Trailing edge noise is simulated based on acoustic perturbation equations and a stochastic model for...
The TE noise radiated by aNACA0012 airfoil, at zero incidence, is studied. The mean turbulent flow p...
AbstractThe current status of a hybrid RANS/CAA approach for the simulation of broadband sound gener...
The long term objective of this project is to develop a computational method for predicting the nois...
An efficient stochastic method is applied to the problem of modelling unsteady turbulent velocity fl...