Characterization of pressure fluctuations within a controlled-diffusion blade boundary layer using the equilibrium wall-modelled LES

R Boukharfane, M Parsani, J Bodart - Scientific reports, 2020 - nature.com
In this study, the generation of airfoil trailing edge broadband noise that arises from the
interaction of turbulent boundary layer with the airfoil trailing edge is investigated. The …

Trailing edge noise prediction based on wall pressure spectrum models for NACA0012 airfoil

YC Küçükosman, J Christophe, C Schram - Journal of Wind Engineering …, 2018 - Elsevier
This paper compares several approaches for the prediction of the noise emitted by a
NACA0012 airfoil at 0∘ and 4∘ of angle of attack and a Reynolds number R e= 1.5× 10 6 …

Numerical study on the noise propagation characteristics of rotor in non-uniform downwash flowfield Based on Linearized Euler Equations

T Yang, X Chen, Q Zhao… - International Journal of …, 2022 - journals.sagepub.com
To study the influence of non-uniform flowfield on the propagation characteristics of
helicopter rotor noise, a Hybrid Computational Aeroacoustics (HCAA) method is developed …

Investigation of the acoustic installation effects of an open-jet anechoic wind tunnel using computational aeroacoustics

S Redonnet - Applied Acoustics, 2020 - Elsevier
This study focuses on acoustic installation effects that may occur during airframe noise
experiments conducted in a typical open-jet anechoic wind tunnel, exemplified here by the …

Low-order aeroacoustic prediction of low-speed axial fan noise

A Zarri, J Christophe, CF Schram - 25th AIAA/CEAS Aeroacoustics …, 2019 - arc.aiaa.org
In the automotive field, the noise emitted by low-speed fans while cooling down the engine
has acquired critical importance for the passengers comfort and because of the international …

Characterization of the pressure fluctuations within a Controlled-Diffusion airfoil boundary layer at large Reynolds numbers

R Boukharfane, J Bodart, MC Jacob, L Joly… - 25th AIAA/CEAS …, 2019 - arc.aiaa.org
The present investigation targets the generation of airfoil trailing-edge broadband noise that
arises from the interaction of turbulent boundary layer with the airfoil trailing edge. Large …

Numerical Study on the Unusual Vibration Load Characteristics and Mechanisms of the Front Landing Gear Compartment

H Dang, J Xu, W Wang, X Wang, B Li, R Cao, L Kang… - Aerospace, 2023 - mdpi.com
Civilian aircraft can experience noticeable vibrations in the cockpit and cabin due to
mechanical faults during flight. To address this issue, a hybrid approach was utilized to …

Adaptation des méthodes et outils aéroacoustiques pour les jets en interaction dans le cadre des lanceurs spatiaux.

A Langenais - 2019 - theses.hal.science
Lors d'un lancement spatial, le bruit des jets supersoniques chauds, générés par les
moteurs-fusées au décollage et en interaction avec le pas de tir, est dommageable pour le …

Further assessment of a time domain impedance boundary condition for the numerical simulation of noise-absorbing materials

S Redonnet - International Journal of Aeroacoustics, 2021 - journals.sagepub.com
In regard to the mitigation of environmental noise across major industry sectors, the present
study focuses on the numerical prediction of passive noise reduction devices. Here, it is …

Numerical Investigation of Noise Reduction Effects of Slat Cusp Sawtooth and Slat Cusp Extension

W Wang, Y Sun - China Aeronautical Science and Technology …, 2023 - Springer
Slat cusp sawtooth and slat cusp extension are both potential small-size low noise devices
on slat cusp, which have advantages of compatibility on certification rules and sturcture …