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Large-eddy simulation of flows over random urban-like obstacles
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 …
cubes, a simulation of flow over random urban-like obstacles is presented. To gain a deeper …
Sub-harmonic broadband humps and tip noise in low-speed ring fans
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 …
in clean inflow. Experimental evidence shows large periodic broadband humps at lower …
Rotating blade trailing-edge noise: Experimental validation of analytical model
Rotating Blade Trailing-Edge Noise: Experimental Validation of Analytical Model Page 1 Rotating
Blade Trailing-Edge Noise: Experimental Validation of Analytical Model Yannick Rozenberg ∗ …
Blade Trailing-Edge Noise: Experimental Validation of Analytical Model Yannick Rozenberg ∗ …
On the noise generated by a controlled-diffusion aerofoil at Rec= 1.5× 105
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 …
Controlled-Diffusion aerofoil at 8∘ geometrical angle of attack, a Reynolds number of R ec …
Angle-of-attack and Mach number effects on the aeroacoustics of an SD7003 airfoil at Reynolds number 60,000
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 …
Large Eddy Simulation. Five simulations are performed to study the effects of angle-of-attack …
Computation of wall pressure spectra from steady flow data for noise prediction
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 aeronautic industry. Because of the strong reduction of jet noise in recent aircraft …
[HTML][HTML] Beamforming based extension of semi-empirical noise modelling for low-speed axial flow fans
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 …
the semi-empirical Brooks-Pope-Marcolini (BPM) model in an axial flow fan case study is …
[PDF][PDF] LES of the trailing-edge flow and noise of a controlled-diffusion airfoil at high angle of attack
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 …
are performed using two different flow solvers, Fluent and CDP, on the same fine structured …
[PDF][PDF] LES of the trailing-edge flow and noise of a NACA6512-63 airfoil at zero angle of attack
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 …
negative incidence is performed using two different flow solvers, CFX and Fluent, on a …
[PDF][PDF] Validation of unstructured-mesh LES of the trailing-edge flow and noise of a controlled-diffusion airfoil
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 …
unstructured-mesh flow solver with an efficient mesh-refinement strategy. Results from three …