Yan, Y., Avital, E., Shen, X., Zhao, Q., Gao, J., Li, X., & Korakianitis, T. (2017). Aerodynamic and aeroacoustic redesign of low speed blade profile. Paper presented at 24th International Congress on Sound and Vibration, ICSV 2017, London, United Kingdom.
Yan, Y. ; Avital, E. ; Shen, X. et al. / Aerodynamic and aeroacoustic redesign of low speed blade profile. Paper presented at 24th International Congress on Sound and Vibration, ICSV 2017, London, United Kingdom.
@conference{230a2ba02c884fb886dc4460e1ade728,
title = "Aerodynamic and aeroacoustic redesign of low speed blade profile",
abstract = "A method to design aerofoils is discussed in order to improve aerodynamic efficiency by removing discontinuities in the curvature and slope of curvature. It is shown to delay stall and flow separation for two low Re-number aerofoils (NACA0012 and E387). Laminar boundary layer tonal noise is shown to be suppressed. Aerodynamic and aeroacoustic performance of the blades used for kinetic turbines is also discussed. Computational and experimental results are analysed.",
keywords = "Aerodynamic efficiency, Circle method, Noise",
author = "Y. Yan and E. Avital and X. Shen and Q. Zhao and J. Gao and X. Li and T. Korakianitis",
year = "2017",
language = "English",
note = "24th International Congress on Sound and Vibration, ICSV 2017 ; Conference date: 23-07-2017 Through 27-07-2017",
}
Yan, Y, Avital, E, Shen, X, Zhao, Q, Gao, J, Li, X & Korakianitis, T 2017, 'Aerodynamic and aeroacoustic redesign of low speed blade profile', Paper presented at 24th International Congress on Sound and Vibration, ICSV 2017, London, United Kingdom, 23/07/17 - 27/07/17.
Aerodynamic and aeroacoustic redesign of low speed blade profile. /
Yan, Y.; Avital, E.; Shen, X. et al.
2017. Paper presented at 24th International Congress on Sound and Vibration, ICSV 2017, London, United Kingdom.
Research output: Contribution to conference › Paper › peer-review
TY - CONF
T1 - Aerodynamic and aeroacoustic redesign of low speed blade profile
AU - Yan, Y.
AU - Avital, E.
AU - Shen, X.
AU - Zhao, Q.
AU - Gao, J.
AU - Li, X.
AU - Korakianitis, T.
PY - 2017
Y1 - 2017
N2 - A method to design aerofoils is discussed in order to improve aerodynamic efficiency by removing discontinuities in the curvature and slope of curvature. It is shown to delay stall and flow separation for two low Re-number aerofoils (NACA0012 and E387). Laminar boundary layer tonal noise is shown to be suppressed. Aerodynamic and aeroacoustic performance of the blades used for kinetic turbines is also discussed. Computational and experimental results are analysed.
AB - A method to design aerofoils is discussed in order to improve aerodynamic efficiency by removing discontinuities in the curvature and slope of curvature. It is shown to delay stall and flow separation for two low Re-number aerofoils (NACA0012 and E387). Laminar boundary layer tonal noise is shown to be suppressed. Aerodynamic and aeroacoustic performance of the blades used for kinetic turbines is also discussed. Computational and experimental results are analysed.
KW - Aerodynamic efficiency
KW - Circle method
KW - Noise
UR - http://www.scopus.com/inward/record.url?scp=85029409218&partnerID=8YFLogxK
M3 - Paper
AN - SCOPUS:85029409218
T2 - 24th International Congress on Sound and Vibration, ICSV 2017
Y2 - 23 July 2017 through 27 July 2017
ER -
Yan Y, Avital E, Shen X, Zhao Q, Gao J, Li X et al.. Aerodynamic and aeroacoustic redesign of low speed blade profile. 2017. Paper presented at 24th International Congress on Sound and Vibration, ICSV 2017, London, United Kingdom.