4.5 Article

Unsteady load mitigation through a passive trailing-edge flap

期刊

JOURNAL OF FLUIDS AND STRUCTURES
卷 106, 期 -, 页码 -

出版社

ACADEMIC PRESS LTD- ELSEVIER SCIENCE LTD
DOI: 10.1016/j.jfluidstructs.2021.103352

关键词

Unsteady aerodynamics; Load alleviation; Unsteady loading; Passive trailing-edge flap; Tidal energy

资金

  1. Wave Energy Scotland (WES) , UK
  2. UK Engineering and Physical Sciences Research Council (EPSRC), UK via the EPSRC Centre for Marine Energy Research, UK [EP/P008682/1]
  3. EPSRC Centre for Advanced Materials for Renewable Energy Generation, UK [EP/P007805/1]
  4. [EP/M02038X/1]
  5. [EP/R511687/1]
  6. EPSRC [EP/P007805/1] Funding Source: UKRI

向作者/读者索取更多资源

Passive trailing-edge flaps can effectively alleviate unsteady load fluctuations by up to 25% without affecting the mean load, with effectiveness dependent on their size relative to the foil.
There are a wide range of applications in which it is desirable to mitigate unsteady load fluctuations while preserving mean loading. This is often achieved with active control systems, but passive systems are sometimes more desirable for enhancing reliability. This is the case, for example, for wind and tidal turbines, where unsteady loading limits the fatigue life of the turbine and results in power peaks at the generator. Here, we consider the unsteady load mitigation that can be achieved through a foil with a trailing edge flap that is connected to the foil via a torsional spring. We develop a theoretical model and show that the preload can be tuned to preserve the mean foil loading. The spring moment that maximises the unsteady load mitigation is approximately constant, and the load fluctuation reduction is linearly proportional to the ratio of the flap to the full chord of the foil. We verify this relationship through water tunnel tests of a foil with a hinge at 25% of the chord from the trailing edge. As theoretically predicted, we measure unsteady load mitigation of up to 25%, without any variation in the mean load. In highly unsteady flow conditions, when boundary layer separation occurs, the unsteady load reduction decreases. Overall we conclude that passive trailing-edge flaps are effective in alleviating unsteady load fluctuations and their effectiveness depends on their size relative to the foil. (C) 2021 Elsevier Ltd. All rights reserved.

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