Design and testing of a deformable wind turbine blade control surface

S. Daynes, P. M. Weaver

Research output: Contribution to journalArticlepeer-review

Abstract

Wind tunnel tests were conducted on a 1.3m chord NACA 63-418 blade section fitted with an adaptive trailing edge flap. The 20% chord flap had an aramid honeycomb core covered with a silicone skin and was actuated using servo motors. The honeycomb core had a high stiffness in the thickness direction but was compliant in chordwise bending. These anisotropic properties offer a potential solution for the conflicting design requirements found in morphing trailing edge structures. Static and dynamic tests were performed up to a Reynolds number of 5.4×10 6. The tests showed that deflecting the flap from -10°to +10°changes the blade section lift coefficient by 1.0 in non-stalled conditions. Dynamic tests showed the flap to be capable of operating up to 9° s -1 using a 15V power supply. A two-dimensional static aeroelastic model of the morphing flap was developed to analyse strains, predict actuator requirements and study fluid-structure interaction effects. The model was used to conduct parametric studies to further improve the flap design. Potential applications include wind turbine blade load alleviation and increased wind energy capture.

Original languageEnglish
Article number105019
JournalSmart Materials and Structures
Volume21
Issue number10
DOIs
Publication statusPublished - Oct 2012
Externally publishedYes

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