TY - GEN
T1 - A Ffowcs Williams-Hawkings numerical aeroacoustic study of varied and fixed-pitch blades of an H-Rotor vertical axis wind turbine
AU - Molatudi, Errol
AU - Kunene, Thokozani Justin
AU - Tartibu, Lagouge Kwanda
N1 - Publisher Copyright:
© The Authors, published by EDP Sciences. This is an open access article distributed under the terms of the Creative Commons Attribution License 4.0 (http://creativecommons.org/licenses/by/4.0/).
PY - 2020
Y1 - 2020
N2 - The effects of sound pressure level at two observation positions of a fixed and varied blade pitch angle at Low-Mach unsteady incompressible Reynolds-Average Navier-Stokes flow approach, on an H-rotor Vertical Axis Wind Turbine. The objective of the study is to compare the noise dissipation and output power/energy of the airfoil blades design of the vertical axis wind turbine in residential zones. The Ffowcs Williams -Hawkings (FHWH) techniques were applied to validate the output noise and vortex shedding of the different angles of attacks (AoA). The study postulated that the time history of the calculated sound pressure level at two observers positions: the aeroacoustic, blade vortex interaction noise, flow separations, dynamic stall experience from varied angled of attacks are found to produces less noise and vortex shedding compared to the fixed angle of attack.
AB - The effects of sound pressure level at two observation positions of a fixed and varied blade pitch angle at Low-Mach unsteady incompressible Reynolds-Average Navier-Stokes flow approach, on an H-rotor Vertical Axis Wind Turbine. The objective of the study is to compare the noise dissipation and output power/energy of the airfoil blades design of the vertical axis wind turbine in residential zones. The Ffowcs Williams -Hawkings (FHWH) techniques were applied to validate the output noise and vortex shedding of the different angles of attacks (AoA). The study postulated that the time history of the calculated sound pressure level at two observers positions: the aeroacoustic, blade vortex interaction noise, flow separations, dynamic stall experience from varied angled of attacks are found to produces less noise and vortex shedding compared to the fixed angle of attack.
KW - Aeroacoustic
KW - Angle-of-Attack
KW - Ffowcs-Hawkings
KW - Sound Pressure level (SPL)
UR - http://www.scopus.com/inward/record.url?scp=85127592721&partnerID=8YFLogxK
U2 - 10.1051/matecconf/202134700013
DO - 10.1051/matecconf/202134700013
M3 - Conference contribution
AN - SCOPUS:85127592721
T3 - 12th South African Conference on Computational and Applied Mechanics, SACAM 2020
BT - 12th South African Conference on Computational and Applied Mechanics, SACAM 2020
A2 - Skatulla, Sebastian
PB - EDP Sciences
T2 - 12th South African Conference on Computational and Applied Mechanics, SACAM 2020
Y2 - 29 November 2021 through 1 December 2021
ER -