A new method for calculating the aerodynamic noise generated by bluff bodies is presented in this paper. The methodology uses two-dimensional, unsteady Reynolds averaged Navier Stokes turbulent flow simulations to calculate the acoustic source terms. To account for turbulent flow effects that are not resolved by the flow simulation, a statistical approach has been developed and applied to introduce narrow band random noise. Spanwise de-correlation of flow information is accounted for using a correction method based on a de-correlation length scale. Curle's compact acoustic analogy is used to calculate the far-field noise. To illustrate the effectiveness of the method, the turbulent flow and noise about two test cases are calculated and comp...
AbstractThe current status of a hybrid RANS/CAA approach for the simulation of broadband sound gener...
A Computational Aeroacoustic (CAA) study is conducted for the simulation of broad- band trailing-ed...
Diploma thesis is focused on computational modelling of aerodynamic noise of flow past a solid body....
The prediction of aerodynamic noise generated by bluff bodies is important for a broad range of tech...
The current status of a Computational Aeroacoustics (CAA) approach to simulate broadband noise is ...
The efficient computation of turbulent airfoil trailing edge noise is important for the cost-effecti...
In this paper an engineering method for the prediction of noise generated by a turbulent flow is pre...
In this work physics-based modelling of bluff-body noise was performed with application to landing g...
Noise generated by turbulent flow past a sharp edge is important in the design of a variety of appli...
Aerodynamic is a branch of fluid dynamics that evaluates the behavior of airflow and its interaction...
The present paper investigates the numerical methods used to predict aerodynamically generated noise...
In this study, a Computational Aeroacoustics (CAA) method is presented for the prediction of trailin...
Abstract. The present paper investigates the case of an airfoil placed in a turbulent jet. The Reyno...
The prediction quality of a fast Computational Aeroacoustics (CAA) approach is studied for noise gen...
In this work a hybrid RANS/CAA methodology is used to predict trailing-edge noise of a controlled-di...
AbstractThe current status of a hybrid RANS/CAA approach for the simulation of broadband sound gener...
A Computational Aeroacoustic (CAA) study is conducted for the simulation of broad- band trailing-ed...
Diploma thesis is focused on computational modelling of aerodynamic noise of flow past a solid body....
The prediction of aerodynamic noise generated by bluff bodies is important for a broad range of tech...
The current status of a Computational Aeroacoustics (CAA) approach to simulate broadband noise is ...
The efficient computation of turbulent airfoil trailing edge noise is important for the cost-effecti...
In this paper an engineering method for the prediction of noise generated by a turbulent flow is pre...
In this work physics-based modelling of bluff-body noise was performed with application to landing g...
Noise generated by turbulent flow past a sharp edge is important in the design of a variety of appli...
Aerodynamic is a branch of fluid dynamics that evaluates the behavior of airflow and its interaction...
The present paper investigates the numerical methods used to predict aerodynamically generated noise...
In this study, a Computational Aeroacoustics (CAA) method is presented for the prediction of trailin...
Abstract. The present paper investigates the case of an airfoil placed in a turbulent jet. The Reyno...
The prediction quality of a fast Computational Aeroacoustics (CAA) approach is studied for noise gen...
In this work a hybrid RANS/CAA methodology is used to predict trailing-edge noise of a controlled-di...
AbstractThe current status of a hybrid RANS/CAA approach for the simulation of broadband sound gener...
A Computational Aeroacoustic (CAA) study is conducted for the simulation of broad- band trailing-ed...
Diploma thesis is focused on computational modelling of aerodynamic noise of flow past a solid body....