In:
Wind Energy Science, Copernicus GmbH, Vol. 8, No. 4 ( 2023-04-06), p. 465-485
Abstract:
Abstract. This paper provides a summary of the work done within Phase III of the Offshore Code Comparison Collaboration, Continued, with Correlation and unCertainty (OC6) project, under the International Energy Agency Wind Technology Collaboration Programme Task 30. This phase focused on validating the aerodynamic loading on a wind turbine rotor undergoing large
motion caused by a floating support structure. Numerical models of the
Technical University of Denmark 10 MW reference wind turbine were validated using measurement data from a 1:75 scale test performed during the UNsteady Aerodynamics for FLOating Wind (UNAFLOW) project and a follow-on experimental campaign, both performed at the Politecnico di Milano wind tunnel. Validation of the models was performed by comparing the loads for steady (fixed platform) and unsteady (harmonic motion of the platform) wind conditions. For the unsteady wind conditions, the platform was forced to oscillate in the surge and pitch directions under several frequencies and amplitudes. These oscillations result in a wind variation that impacts the rotor loads (e.g., thrust and torque). For the conditions studied in these tests, the system aerodynamic response was almost steady. Only a small hysteresis in airfoil performance undergoing angle of attack variations in attached flow was observed. During the experiments, the rotor speed and blade pitch angle were held constant. However, in real wind turbine operating conditions, the surge and pitch variations would result in rotor speed variations and/or blade pitch actuations, depending on the wind turbine controller region that the system is operating. Additional
simulations with these control parameters were conducted to verify the
fidelity of different models. Participant results showed, in general, a good
agreement with the experimental measurements and the need to account for
dynamic inflow when there are changes in the flow conditions due to the
rotor speed variations or blade pitch actuations in response to surge and
pitch motion. Numerical models not accounting for dynamic inflow effects
predicted rotor loads that were 9 % lower in amplitude during rotor speed
variations and 18 % higher in amplitude during blade pitch actuations.
Type of Medium:
Online Resource
ISSN:
2366-7451
DOI:
10.5194/wes-8-465-2023
Language:
English
Publisher:
Copernicus GmbH
Publication Date:
2023
detail.hit.zdb_id:
2846783-8
