The dataset the results of a detailed experimental investigation into the effectiveness of sinusoidal leading edge serrations on aerofoils for the reduction of the noise generated by the interaction with turbulent flow. The data underpins the paper P. Chaitanya?, P. Joseph, S. Narayanan?, C. Vanderwel, J. Turner, J. W. Kim, and B. Ganapathisubramani (2017), 'Performance and mechanism of sinusoidal leading edge serrations for the reduction of turbulence-aerofoil interaction noise', accepted in the Journal of Fluid Mechanics.</span
The present work is aimed at assessing leading-edge serrations as an airfoil turbulenceimpingement n...
This paper presents the preliminary results on the aeroacoustic and aerodynamic performances of a NA...
With the objective of reducing the broadband noise, emitted from the interaction of highly turbulent...
Aerofoils operating in a turbulent flow are an efficient source of noise radiation by scattering vor...
Sinusoidal leading edge serrations of a cambered NACA65(12)-10 aerofoil were analysed with the aim o...
Aerofoils operating in a turbulent flow are an efficient source of noise radiation by scattering vor...
Aerofoils operating in a turbulent flow are an efficient source of noise radiation by scattering vor...
Aerofoils operating in a turbulent flow are an efficient source of noise radiation by scattering vor...
Turbulent flow interaction with the leading edge of an airfoil generates a well-known leading edge n...
Aerofoils operating in a turbulent flow generate broadband noise by scattering vorticity into sound ...
Aerofoils operating in a turbulent flow generate broadband noise by scattering vorticity into sound ...
Aerofoils operating in a turbulent flow generate broadband noise by scattering vorticity into sound ...
This paper provides an experimental investigation into the use of leading edge (LE) serrations as a ...
The present work is aimed at assessing leading-edge serrations as an airfoil turbulenceimpingement n...
The data supports the paper by Kim, Haeri & Joseph (2016) 'On the reduction of aerofoil-turb...
The present work is aimed at assessing leading-edge serrations as an airfoil turbulenceimpingement n...
This paper presents the preliminary results on the aeroacoustic and aerodynamic performances of a NA...
With the objective of reducing the broadband noise, emitted from the interaction of highly turbulent...
Aerofoils operating in a turbulent flow are an efficient source of noise radiation by scattering vor...
Sinusoidal leading edge serrations of a cambered NACA65(12)-10 aerofoil were analysed with the aim o...
Aerofoils operating in a turbulent flow are an efficient source of noise radiation by scattering vor...
Aerofoils operating in a turbulent flow are an efficient source of noise radiation by scattering vor...
Aerofoils operating in a turbulent flow are an efficient source of noise radiation by scattering vor...
Turbulent flow interaction with the leading edge of an airfoil generates a well-known leading edge n...
Aerofoils operating in a turbulent flow generate broadband noise by scattering vorticity into sound ...
Aerofoils operating in a turbulent flow generate broadband noise by scattering vorticity into sound ...
Aerofoils operating in a turbulent flow generate broadband noise by scattering vorticity into sound ...
This paper provides an experimental investigation into the use of leading edge (LE) serrations as a ...
The present work is aimed at assessing leading-edge serrations as an airfoil turbulenceimpingement n...
The data supports the paper by Kim, Haeri & Joseph (2016) 'On the reduction of aerofoil-turb...
The present work is aimed at assessing leading-edge serrations as an airfoil turbulenceimpingement n...
This paper presents the preliminary results on the aeroacoustic and aerodynamic performances of a NA...
With the objective of reducing the broadband noise, emitted from the interaction of highly turbulent...