Results 21 to 30 of about 21,854 (248)

On the Application of Wavelet Transform in Jet Aeroacoustics

open access: yesFluids, 2021
Wavelet transform has become a common tool for processing non-stationary signals in many different fields. The present paper reports a review of some applications of wavelet in aeroacoustics with a special emphasis on the analysis of experimental data ...
R. Camussi, S. Meloni
semanticscholar   +1 more source

Lattice Boltzmann method for computational aeroacoustics on non-uniform meshes: A direct grid coupling approach [PDF]

open access: yesJournal of Computational Physics, 2020
The present study proposes a highly accurate lattice Boltzmann direct coupling cell-vertex algorithm, well suited for industrial purposes, making it highly valuable for aeroacoustic applications.
Thomas Astoul   +4 more
semanticscholar   +1 more source

Comparison of outflow boundary conditions for subsonic aeroacoustic simulations [PDF]

open access: yes, 2011
Aeroacoustics simulations require much more precise boundary conditions than classical aerodynamics. Two classes of non-reflecting boundary conditions for aeroacoustics are compared in the present work: characteristic analysis based methods and Tam and ...
Berenger   +23 more
core   +3 more sources

Aeroacoustics research in Europe: The CEAS-ASC report on 2019 highlights

open access: yesJournal of Sound and Vibration, 2020
The Council of European Aerospace Societies (CEAS) Aeroacoustics Specialists Committee (ASC) supports and promotes the interests of the scientific and industrial aeroacoustics community on a European scale and European aeronautics activities ...
R. Camussi, G. Bennett
semanticscholar   +1 more source

Reduced dimension modeling of leading edge turbulent interaction noise [PDF]

open access: yes, 2014
A computational aeroacoustics approach is used to model the effects of real airfoil geometry on leading edge turbulent interaction noise for symmetric airfoils at zero angle of attack.
Bailly C.   +5 more
core   +1 more source

On the effect of the tip-clearance ratio on the aeroacoustics of a diffuser-augmented wind turbine

open access: yesRenewable Energy, 2020
Lattice-Boltzmann Very-Large-Eddy Simulations of two Diffuser-Augmented Wind Turbines are carried out to investigate the effect of the tip-clearance (TC) ratio on both the flow field and the far-field noise. The DonQi® wind turbine, a three blades ducted
F. Avallone, D. Ragni, D. Casalino
semanticscholar   +1 more source

Numerical and Experimental Investigations of Axial Flow Fan with Bionic Forked Trailing Edge

open access: yesMachines, 2023
To improve the performance of the aerodynamic properties and reduce the aerodynamic noise of an axial flow fan in the outdoor unit of an air conditioner, this study proposed a bionic forked trailing-edge structure inspired by the forked fish caudal fin ...
Zhong Liang   +5 more
doaj   +1 more source

Residual-based stabilization of the finite element approximation to the acoustic perturbation equations for low Mach number aeroacoustics [PDF]

open access: yes, 2016
This is the peer reviewed version of the following article: [Guasch, O., Sánchez-Martín, P., Pont, A., Baiges, J., and Codina, R. (2016) Residual-based stabilization of the finite element approximation to the acoustic perturbation equations for low Mach ...
Baiges Aznar, Joan   +4 more
core   +3 more sources

Computational aeroacoustics of the EAA benchmark case of an axial fan

open access: yesActa Acustica, 2020
This contribution benchmarks the aeroacoustic workflow of the perturbed convective wave equation and the Ffowcs Williams and Hawkings analogy in Farassat’s 1A version for a low-pressure axial fan.
S. Schoder   +2 more
semanticscholar   +1 more source

Experimental Investigations on the Possibility to Apply the Corrugated Sheet Metal Used in the Past with Junkers Aircraft to Reduce Noise for Future European Aircraft. Other Noise Reduction Experiments for Future European Aircraft [PDF]

open access: yesINCAS Bulletin, 2018
This paper shows that corrugated skin used in the past with Junkers aircraft to increase the fuselage and wing rigidity can lead to noise reduction for future European aircraft. If the pressure side of wing which is placed above the engine is corrugated,
Constantin SANDU   +4 more
doaj   +1 more source

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