[HTML][HTML] Turbulent boundary layer trailing-edge noise: Theory, computation, experiment, and application

S Lee, L Ayton, F Bertagnolio, S Moreau… - Progress in Aerospace …, 2021 - Elsevier
When the pressure fluctuations caused by turbulence vorticity in the boundary layer are
scattered by a sharp trailing edge, acoustic energy is generated and propagated to the far …

Challenges and opportunities for low noise electric aircraft

E Greenwood, KS Brentner, RF Rau… - International Journal …, 2022 - journals.sagepub.com
A new class of electric aircraft is being developed to transport people and goods as a part of
the urban and regional transportation infrastructure. To gain public acceptance of these …

The third golden age of aeroacoustics

S Moreau - Physics of Fluids, 2022 - pubs.aip.org
The present review covers the latest evolution of computational aeroacoustics, the field that
deals with the noise generated by fluid flows and its propagation in the medium. It highlights …

[PDF][PDF] Numerical investigation of leading edge noise reduction on a rod-airfoil configuration using porous materials and serrations

C Teruna, F Avallone, D Casalino, D Ragni - J. Sound Vib, 2021 - core.ac.uk
abstract A lattice-Boltzmann method has been employed to study the aeroacoustics and
aerodynamics of airfoils equipped with leading edge treatments, namely the porous leading …

Relevance of quadrupolar sound diffraction on flow-induced noise from porous-coated cylinders

R Zamponi, F Avallone, D Ragni, C Schram… - Journal of Sound and …, 2024 - Elsevier
This paper elucidates the link between the near-wake development of a circular cylinder
coated with a porous material in a low Mach-number flow and the related aerodynamic …

Permeable leading edges for airfoil and fan noise reduction in disturbed inflow

C Ocker, TF Geyer, F Czwielong, F Krömer, W Pannert… - AIAA Journal, 2021 - arc.aiaa.org
A detailed experimental study on the aerodynamic performance and noise emission of
airfoils and fan blades with permeable leading edges under disturbed inflow conditions was …

[HTML][HTML] Inflow turbulence distortion for airfoil leading-edge noise prediction for large turbulence length scales for zero-mean loading

FL Dos Santos, L Botero-Bolívar, CH Venner… - The Journal of the …, 2023 - pubs.aip.org
Turbulence distortion due to airfoil finite thickness is an important but not fully understood
phenomenon that affects the airfoil radiated noise, resulting in inaccurate noise predictions …

[HTML][HTML] Effect of porosity on Curle's dipolar sources on an aerofoil in turbulent flow

R Zamponi, S Satcunanathan, S Moreau… - Journal of Sound and …, 2023 - Elsevier
Integrating a porous material into the structure of an aerofoil constitutes a promising passive
strategy for mitigating the noise from turbulence–body interactions that has been extensively …

[HTML][HTML] Downstream porosity for the reduction of turbulence–aerofoil interaction noise

S Palleja-Cabre, P Chaitanya, P Joseph, JW Kim… - Journal of Sound and …, 2022 - Elsevier
This paper is a predominantly experimental study into the use of porosity located
downstream of an aerofoil leading edge for the reduction of turbulence interaction noise …

[HTML][HTML] Recent advances in airfoil self-noise passive reduction

B Amirsalari, J Rocha - Aerospace, 2023 - mdpi.com
Airflow-induced noise prediction and reduction is one of the priorities for both the energy
and aviation industries. This review paper provides valuable insights into flow-induced noise …