2020
DOI: 10.5194/wes-5-1537-2020
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Identification of airfoil polars from uncertain experimental measurements

Abstract: Abstract. A new method is described to identify the aerodynamic characteristics of blade airfoils directly from operational data of the turbine. Improving on a previously published approach, the present method is based on a new maximum likelihood formulation that includes errors in both the outputs and the inputs, generalizing the classical error-in-the-outputs-only formulation. Since many parameters are necessary to meaningfully represent the behavior of airfoil polars as functions of angle of attack and Reyn… Show more

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Cited by 10 publications
(6 citation statements)
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“…The inflow observer described in [17] is used to estimate the local wind speed at each turbine. The method, which has been validated with wind tunnel [18] and field [19] data, employs the power C P and the cone C m coefficients of the G1, derived with the Blade Element Momentum (BEM) model described in [20]. The C P and C m are used to compute lookup tables (LUTs) that return the local wind speed at the azimuthal position occupied by a blade, given the aerodynamic torque and the two out-of-plane bending moments measured on the shaft, as well as the measured rotor speed, blade pitch, and air density.…”
Section: Measured and Estimated Quantitiesmentioning
confidence: 99%
“…The inflow observer described in [17] is used to estimate the local wind speed at each turbine. The method, which has been validated with wind tunnel [18] and field [19] data, employs the power C P and the cone C m coefficients of the G1, derived with the Blade Element Momentum (BEM) model described in [20]. The C P and C m are used to compute lookup tables (LUTs) that return the local wind speed at the azimuthal position occupied by a blade, given the aerodynamic torque and the two out-of-plane bending moments measured on the shaft, as well as the measured rotor speed, blade pitch, and air density.…”
Section: Measured and Estimated Quantitiesmentioning
confidence: 99%
“…The error in u pitot is related to the uncertainty associated with the measurements of flow density and dynamic pressure. This latter is measured with a MKS Baratron-Type 226A transducer (Baratron, 2022) with full span equal to 1 Torr, characterized by an accuracy of ±0.4 Pa. Density is instead derived from measurements of air pressure, temperature and humidity, and it is affected by an error equal to ±0.01 kgm 3 (Wang et al, 2020). Torque is measured with a load cell installed on the rotor shaft, and it is affected by an uncertainty of ±0.005 Nm.…”
Section: Wind Tunnel Measurementsmentioning
confidence: 99%
“…The measurement uncertainty on power P = QΩ is derived by adding in quadrature the uncertainties on Q and Ω. Finally, thrust T is obtained by correcting the measurements of the bending moments at tower base by the effects induced by the drag of the tower, nacelle and hub spinner (Wang et al, 2020). The calibration of the load cell at tower base reveled an uncertainty on the thrust of ±0.14 N. In turn, all these effects are used to quantify uncertainties in the tip speed ratio λ, thrust coefficient C T , and yaw-induced power losses η P , again by adding errors in quadrature.…”
Section: Wind Tunnel Measurementsmentioning
confidence: 99%
“…By this method, the nominal polars are corrected, resulting in tuned aerodynamic characteristics that better reflect the actual conditions on the manufactured rotor. This maximum-likelihood calibration procedure was further improved in Wang et al (2020b), to better account for measurement errors.…”
Section: Numerical Simulations: Polar Identificationmentioning
confidence: 99%