We are now at a point where airframes, aeroengines and their integration require radical
changes to meet increasingly aggressive environmental targets. Generally, fan noise …

The present paper is aimed at providing an updated review of prediction methods for the
aerodynamic noise of ducted rotor–stator stages. Indeed, ducted rotating-blade technologies …

Large-eddy simulation is combined with the Ffowcs Williams–Hawkings equation to
investigate the noise generation by a 10-bladed rotor ingesting the turbulent wake of a …

The turbulent boundary layer over a Gaussian bump is computed by direct numerical
simulation (DNS) and wall-modeled large eddy simulation (WMLES) of the incompressible …

The fan broadband noise of a rotor–stator system representing a turbofan aeroengine is
investigated using the improved delayed detached-eddy-simulation approach. The baseline …

Large Eddy Simulation is performed using the NASA Source Diagnostic Test turbofan at
approach conditions (62% of the design speed). The simulation is performed in a periodic …

The Ffowcs Williams–Hawkings equation is widely used in computational aeroacoustics to
post-process unsteady simulations and provide the sound at distances beyond the accurate …

Hydrodynamic instabilities in the interstage of turbomachinery and their relation to fan
broadband noise are investigated over wide operating conditions. By applying compressible …

The Paper presents the aerodynamic and turbulent aspects of a project devoted to creating
and validating a high-fidelity computational-fluid-dynamics-based system for the prediction …

The acoustic response of a five-bladed rotor to an axisymmetric turbulent boundary layer at
the tail end of a body of revolution (BOR) is investigated numerically to elucidate the …