The trailing edge of a NACA 0018 airfoil is modified through the attachment of serrations with different degrees of permeability. Acoustic beamforming is used to inspect the turbulent boundary layer-trailing edge noise emissions from the unmodified and serrated trailing edges. Different freestream velocities and angles of attack are investigated. The serration permeability is prescribed by having slits cut into the solid surface of the serrations in two different configurations. The results indicate that a certain benefit in noise reduction is obtained from a mixed solid/slitted configuration, while a fully slitted configuration loses most of the noise reduction performance
The main objective of the present work is to investigate the mechanism of trailing-edge airfoil nois...
Direct numerical simulations of the flow around a NACA-0012 aerofoil are conducted, employing an imm...
The goal of this paper is to perform a detailed analysis of the hydrodynamic near field and acoustic...
The trailing edge of a NACA 0018 airfoil is modified through the attachment of serrations with diffe...
Trailing edge serrations designed to reduce airfoil self-noise are retrofitted on a NACA 0018 airfoi...
Trailing edge serrations designed to reduce airfoil self-noise are retrofitted on a NACA 0018 airfoi...
The paper presents an experimental investigation of a turbulent boundary-layer interaction over a si...
<p>The broadband noise generated by the scattering of turbulent flow at the trailing edge of a NACA ...
The present work investigates the broadband noise reduction that can be achieved using trailing-edge...
The broadband noise generated by the scattering of turbulent flow at the trailing edge of a NACA 001...
The present study investigates the efficacy of sinusoidal trailing-edge (TE) serrations as a passive...
DNS of the flow around a NACA-0012 airfoil are conducted, employing an immersedboundary method to re...
The presentation summarizes the outcome from recent measurements in the Acoustic Wind-Tunnel Braunsc...
International audienceThis study aims at investigating the noise reduction potential of trailing edg...
International audienceThis study aims at investigating the noise reduction potential of trailing edg...
The main objective of the present work is to investigate the mechanism of trailing-edge airfoil nois...
Direct numerical simulations of the flow around a NACA-0012 aerofoil are conducted, employing an imm...
The goal of this paper is to perform a detailed analysis of the hydrodynamic near field and acoustic...
The trailing edge of a NACA 0018 airfoil is modified through the attachment of serrations with diffe...
Trailing edge serrations designed to reduce airfoil self-noise are retrofitted on a NACA 0018 airfoi...
Trailing edge serrations designed to reduce airfoil self-noise are retrofitted on a NACA 0018 airfoi...
The paper presents an experimental investigation of a turbulent boundary-layer interaction over a si...
<p>The broadband noise generated by the scattering of turbulent flow at the trailing edge of a NACA ...
The present work investigates the broadband noise reduction that can be achieved using trailing-edge...
The broadband noise generated by the scattering of turbulent flow at the trailing edge of a NACA 001...
The present study investigates the efficacy of sinusoidal trailing-edge (TE) serrations as a passive...
DNS of the flow around a NACA-0012 airfoil are conducted, employing an immersedboundary method to re...
The presentation summarizes the outcome from recent measurements in the Acoustic Wind-Tunnel Braunsc...
International audienceThis study aims at investigating the noise reduction potential of trailing edg...
International audienceThis study aims at investigating the noise reduction potential of trailing edg...
The main objective of the present work is to investigate the mechanism of trailing-edge airfoil nois...
Direct numerical simulations of the flow around a NACA-0012 aerofoil are conducted, employing an imm...
The goal of this paper is to perform a detailed analysis of the hydrodynamic near field and acoustic...