Parked aeroelastic field rotor response for a 20% scaled demonstrator of a 13‐MW downwind turbine

Abstract Aeroelastic parked testing of a unique downwind two‐bladed subscale rotor was completed to characterize the response of an extreme‐scale 13‐MW turbine in high‐wind parked conditions. A 20% geometric scaling was used resulting in scaled 20‐m‐long blades, whose structural and stiffness proper...

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Main Authors: Meghan Kaminski, Eric Loth, Lee Jay Fingersh, Andy Scholbrock, Michael Selig
Format: Article
Language:English
Published: Wiley 2023-02-01
Series:Wind Energy
Subjects:
Online Access:https://doi.org/10.1002/we.2794
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author Meghan Kaminski
Eric Loth
Lee Jay Fingersh
Andy Scholbrock
Michael Selig
author_facet Meghan Kaminski
Eric Loth
Lee Jay Fingersh
Andy Scholbrock
Michael Selig
author_sort Meghan Kaminski
collection DOAJ
description Abstract Aeroelastic parked testing of a unique downwind two‐bladed subscale rotor was completed to characterize the response of an extreme‐scale 13‐MW turbine in high‐wind parked conditions. A 20% geometric scaling was used resulting in scaled 20‐m‐long blades, whose structural and stiffness properties were designed using aeroelastic scaling to replicate the nondimensional structural aeroelastic deflections and dynamics that would occur for a lightweight, downwind 13‐MW rotor. The subscale rotor was mounted and field tested on the two‐bladed Controls Advanced Research Turbine (CART2) at the National Renewable Energy Laboratory's Flatiron Campus (NREL FC). The parked testing of these highly flexible blades included both pitch‐to‐run and pitch‐to‐feather configurations with the blades in the horizontal braked orientation. The collected experimental data includes the unsteady flapwise root bending moments and tip deflections as a function of inflow wind conditions. The bending moments are based on strain gauges located in the root section, whereas the tip deflections are captured by a video camera on the hub of the turbine pointed toward the tip of the blade. The experimental results are compared against computational predictions generated by FAST, a wind turbine simulation software, for the subscale and full‐scale models with consistent unsteady wind fields. FAST reasonably predicted the bending moments and deflections of the experimental data in terms of both the mean and standard deviations. These results demonstrate the efficacy of the first such aeroelastically scaled turbine test and demonstrate that a highly flexible lightweight downwind coned rotor can be designed to withstand extreme loads in parked conditions.
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spelling doaj.art-afbb94c32f344ae4ac07950040c4e53e2023-01-12T07:11:10ZengWileyWind Energy1095-42441099-18242023-02-0126218220010.1002/we.2794Parked aeroelastic field rotor response for a 20% scaled demonstrator of a 13‐MW downwind turbineMeghan Kaminski0Eric Loth1Lee Jay Fingersh2Andy Scholbrock3Michael Selig4Department of Mechanical and Aerospace Engineering University of Virginia Charlottesville Virginia USADepartment of Mechanical and Aerospace Engineering University of Virginia Charlottesville Virginia USANational Renewable Energy Laboratory Golden Colorado USANational Renewable Energy Laboratory Golden Colorado USAUniversity of Illinois at Urbana‐Champaign Urbana Illinois USAAbstract Aeroelastic parked testing of a unique downwind two‐bladed subscale rotor was completed to characterize the response of an extreme‐scale 13‐MW turbine in high‐wind parked conditions. A 20% geometric scaling was used resulting in scaled 20‐m‐long blades, whose structural and stiffness properties were designed using aeroelastic scaling to replicate the nondimensional structural aeroelastic deflections and dynamics that would occur for a lightweight, downwind 13‐MW rotor. The subscale rotor was mounted and field tested on the two‐bladed Controls Advanced Research Turbine (CART2) at the National Renewable Energy Laboratory's Flatiron Campus (NREL FC). The parked testing of these highly flexible blades included both pitch‐to‐run and pitch‐to‐feather configurations with the blades in the horizontal braked orientation. The collected experimental data includes the unsteady flapwise root bending moments and tip deflections as a function of inflow wind conditions. The bending moments are based on strain gauges located in the root section, whereas the tip deflections are captured by a video camera on the hub of the turbine pointed toward the tip of the blade. The experimental results are compared against computational predictions generated by FAST, a wind turbine simulation software, for the subscale and full‐scale models with consistent unsteady wind fields. FAST reasonably predicted the bending moments and deflections of the experimental data in terms of both the mean and standard deviations. These results demonstrate the efficacy of the first such aeroelastically scaled turbine test and demonstrate that a highly flexible lightweight downwind coned rotor can be designed to withstand extreme loads in parked conditions.https://doi.org/10.1002/we.2794downwindextreme‐scalefield testingflexible bladesgravo‐aeroelastic scalingparked
spellingShingle Meghan Kaminski
Eric Loth
Lee Jay Fingersh
Andy Scholbrock
Michael Selig
Parked aeroelastic field rotor response for a 20% scaled demonstrator of a 13‐MW downwind turbine
Wind Energy
downwind
extreme‐scale
field testing
flexible blades
gravo‐aeroelastic scaling
parked
title Parked aeroelastic field rotor response for a 20% scaled demonstrator of a 13‐MW downwind turbine
title_full Parked aeroelastic field rotor response for a 20% scaled demonstrator of a 13‐MW downwind turbine
title_fullStr Parked aeroelastic field rotor response for a 20% scaled demonstrator of a 13‐MW downwind turbine
title_full_unstemmed Parked aeroelastic field rotor response for a 20% scaled demonstrator of a 13‐MW downwind turbine
title_short Parked aeroelastic field rotor response for a 20% scaled demonstrator of a 13‐MW downwind turbine
title_sort parked aeroelastic field rotor response for a 20 scaled demonstrator of a 13 mw downwind turbine
topic downwind
extreme‐scale
field testing
flexible blades
gravo‐aeroelastic scaling
parked
url https://doi.org/10.1002/we.2794
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