2005
DOI: 10.1115/1.2035700
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Modeling of Aerodynamically Generated Noise From Wind Turbines

Abstract: A semiempirical acoustic generation model based on the work of Brooks, Pope, and Marcolini [NASA Reference Publication 1218 (1989)] has been developed to predict aerodynamic noise from wind turbines. The model consists of dividing the blades of the wind turbine into two-dimensional airfoil sections and predicting the total noise emission as the sum of the contribution from each blade element. Input is the local relative velocities and boundary layer parameters. These quantities are obtained by combining the mo… Show more

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Cited by 85 publications
(72 citation statements)
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“…However, the trend continues to remain the same for all octave band frequencies which is lower in upwind and downwind directions and higher in cross wind directions. This behavior is in contrast to the high and low frequency directivity pattern [3,5,21] observed where sound pressure levels are lower in cross wind receiver positions. It must be noted that receiver heights and distance between the source and receiver are kept constant throughout for qualitative reasons.…”
Section: Mach Number and Rotor Rpmcontrasting
confidence: 40%
See 1 more Smart Citation
“…However, the trend continues to remain the same for all octave band frequencies which is lower in upwind and downwind directions and higher in cross wind directions. This behavior is in contrast to the high and low frequency directivity pattern [3,5,21] observed where sound pressure levels are lower in cross wind receiver positions. It must be noted that receiver heights and distance between the source and receiver are kept constant throughout for qualitative reasons.…”
Section: Mach Number and Rotor Rpmcontrasting
confidence: 40%
“…At 10% of radius (R), the Mach number is least and at 95% of radius the Mach number is highest. The inflow noise magnitude is insignificant for low Mach number flows compared to trailing edge noise [9,15,21] at high frequency. For a wind turbine, when the blades move past the tower, the reduction in relative velocity occurs due to presence of tower.…”
Section: Mach Number and Rotor Rpmmentioning
confidence: 99%
“…The model determines the surface pressure fluctuations using the airfoil's lift response and the turbulent energy spectrum normal to the blade and these fluctuations are then propagated to the far-field as sound. It uses a large aspect-ratio, thin airfoil approximation, and while corrections for airfoil shape, thickness and backscattering have been developed they are not yet widely implemented (Moriarty et al 2005, Roger & Moreau 2005, Zhu et al 2005. Predicted and experimental spectrum differ by less than 6dB for frequencies below 1.5kHz, above this however the accuracy of the model appears to decline rapidly (Amiet 1975, Schlinker & Amiet 1983).…”
Section: Turbulent-inflow Noisementioning
confidence: 99%
“…Figure 1 shows that it has a good lift to drag ratio but is likely to produce less power than the SG6043. The noise analysis is that used by Clifton-Smith (2010) which was based on the semi-empirical formulation of Zhu et al (2005). This objective function will not be described in detail as it is not used in this study.…”
Section: Introductionmentioning
confidence: 99%