AbstractA theoretical model is constructed to predict the far-field sound generated by high-frequency gust–aerofoil interaction in steady parallel shear flow, including the effects of aerofoil thickness. Our approach is to use asymptotic analysis of the Euler equations linearised about steady parallel shear flow, in the limits of high frequency and small, but non-zero, aerofoil thickness and Mach number. The analysis splits the flow into various regions around the aerofoil; local inner regions around the leading and the trailing edges where sound is generated and scattered; a surface transition region accounting for the curvature of the aerofoil; a wake transition region downstream of the aerofoil; and an outer region through which the soun...
This paper presents an analytic solution for the sound generated by an unsteady gust interacting wit...
High-order computational aeroacoustic methods are applied to the modeling of noise due to interactio...
This paper investigates the effects of local leading-edge geometry on unsteady aerofoil interaction ...
A theoretical model is constructed to predict the far-field sound generated by high-frequency gust-a...
An analytic model is created to explore the far-field high-frequency acoustic radiation generated by...
A theory is developed for the influence of airfoil thickness on sound generated by the interaction o...
This thesis considers the sound generated by unsteady perturbations interacting with solid aerofoil...
An analytic solution is obtained for the sound generated by gust-aerofoil interaction for aerofoils ...
Abstract A theoretical model is developed for the sound scattered when a sound wave is incident on a...
This dissertation investigates the effect of airfoil steady loading on the sound generated by the in...
The method of matched asymptotic expansions is used to describe the sound generated by the interacti...
The sound produced by airfoil-gust interaction is a significant source of broadband noise in turbofa...
This paper concerns the calculation of the sound fields which are generated when a vortical gust, co...
The aim of this paper is to survey a range of applications of high-frequency asymptotic methods in a...
Numerical simulations are conducted to investigate the impacts of airfoil thickness, the angle of at...
This paper presents an analytic solution for the sound generated by an unsteady gust interacting wit...
High-order computational aeroacoustic methods are applied to the modeling of noise due to interactio...
This paper investigates the effects of local leading-edge geometry on unsteady aerofoil interaction ...
A theoretical model is constructed to predict the far-field sound generated by high-frequency gust-a...
An analytic model is created to explore the far-field high-frequency acoustic radiation generated by...
A theory is developed for the influence of airfoil thickness on sound generated by the interaction o...
This thesis considers the sound generated by unsteady perturbations interacting with solid aerofoil...
An analytic solution is obtained for the sound generated by gust-aerofoil interaction for aerofoils ...
Abstract A theoretical model is developed for the sound scattered when a sound wave is incident on a...
This dissertation investigates the effect of airfoil steady loading on the sound generated by the in...
The method of matched asymptotic expansions is used to describe the sound generated by the interacti...
The sound produced by airfoil-gust interaction is a significant source of broadband noise in turbofa...
This paper concerns the calculation of the sound fields which are generated when a vortical gust, co...
The aim of this paper is to survey a range of applications of high-frequency asymptotic methods in a...
Numerical simulations are conducted to investigate the impacts of airfoil thickness, the angle of at...
This paper presents an analytic solution for the sound generated by an unsteady gust interacting wit...
High-order computational aeroacoustic methods are applied to the modeling of noise due to interactio...
This paper investigates the effects of local leading-edge geometry on unsteady aerofoil interaction ...