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 …

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 …

In this contribution, a hybrid zonal simulation tool with volumetric inflow turbulence forcing is
applied to trailing-edge noise of a NACA0012 airfoil with and without a porous insert at …

A generalized approach to decompose the compressible Navier-Stokes equations into an
equivalent set of coupled equations for flow and acoustics is introduced. As a significant …

A correction model is presented for sensor-size-related high-frequency attenuation when
measuring the wall pressure fluctuations beneath turbulent boundary layers. The model is …

The Benchmark for Airframe Noise Computations (BANC) has been initiated by the BECAN
Technical Discussion Group under AIAA. This continuous framework, mainly impulsed by …

Experimental results on trailing-edge (TE) noise from a NACA 63 3–018 airfoil are presented
for a chord-based Reynolds number R ec range between 2× 10 5 and 3× 10 6. Far-field TE …

Abstract The Council of European Aerospace Societies (CEAS) Aeroacoustics Specialists
Committee (ASC) supports and promotes the interests of the scientific and industrial …

This paper presents the predictions of airfoil turbulent boundary-layer trailing-edge noise
using empirical wall-pressure spectrum models. Five empirical wall-pressure spectrum …

In a number of institutions and companies, researchers and engineers are developing
modeling numerical frameworks that are used to predict the aerodynamic noise emission …