Further to our previous large-eddy simulation (LES) of flow over a staggered array of uniform
cubes, a simulation of flow over random urban-like obstacles is presented. To gain a deeper …

A joint experimental and numerical study has been achieved on a low-speed axial ring fan
in clean inflow. Experimental evidence shows large periodic broadband humps at lower …

Rotating Blade Trailing-Edge Noise: Experimental Validation of Analytical Model Page 1 Rotating
Blade Trailing-Edge Noise: Experimental Validation of Analytical Model Yannick Rozenberg ∗ …

A compressible direct numerical simulation of the flow and near-field acoustics over a
Controlled-Diffusion aerofoil at 8∘ geometrical angle of attack, a Reynolds number of R ec …

The aeroacoustics of an SD7003 airfoil at Reynolds number 60,000 is investigated using
Large Eddy Simulation. Five simulations are performed to study the effects of angle-of-attack …

BROADBAND noise generated by wall-bounded flows is subject to an increasing interest in
the aeronautic industry. Because of the strong reduction of jet noise in recent aircraft …

The application of the turbulent boundary layer trailing edge (TBL-TE) noise component of
the semi-empirical Brooks-Pope-Marcolini (BPM) model in an axial flow fan case study is …

Large-eddy simulations (LES) of flow over a low-speed airfoil at high angle of attack (15◦)
are performed using two different flow solvers, Fluent and CDP, on the same fine structured …

Large-eddy simulations (LES) of flow over a low-speed highly cambered airfoil at small
negative incidence is performed using two different flow solvers, CFX and Fluent, on a …

Large-Eddy Simulations (LES) of flow over a low-speed airfoil is performed using an
unstructured-mesh flow solver with an efficient mesh-refinement strategy. Results from three …