Aeroelastic model validation of an Active Trailing Edge Flap System tested on a 4.3 MW wind turbine

نویسندگان

چکیده

Abstract Active Trailing Edge Flap Systems (ATEFS) have shown promising results on reducing Wind Turbine fatigue and ultimate loads increasing the Annual Energy Production. However, current lack of field validation creates uncertainty in fidelity level accuracy engineering models used for aeroelastic modeling active flaps, these systems actual load reduction capabilities are question. This article describes based data ATEFS developed BEM-based solvers HAWC2 BHawC case stationary activation flap. The is test from a 4.3 MW with one blade equipped an operating normal power production. With simulation differing measurement max ±3% mean power, ±0.2 deg pitch angle, ±0.1 rpm rotor speed, ±2% flapwise loads, study showed BHAWC provide reliable precise estimation impact

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ژورنال

عنوان ژورنال: Journal of physics

سال: 2022

ISSN: ['0022-3700', '1747-3721', '0368-3508', '1747-3713']

DOI: https://doi.org/10.1088/1742-6596/2265/3/032014