2018
DOI: 10.1007/s13369-018-3270-7
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Improvement of Energy Extraction Efficiency for Flapping Airfoils by Using Oscillating Gurney Flaps

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Cited by 9 publications
(3 citation statements)
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“…Another way to improve extraction efficiency can also be achieved by creating an effective camber which will produce a lift enhancement that is associated with the output power. This concept was studied by Bouzaher et al [29], who added a Gurney flap at the trailing-edge that when synchronized with the flapping motion at a Re = 1100 created this virtual camber that improved the output power. The lift production can be further improved by controlling the development of the leading-edge vortex than, when attached to the airfoil surface, contributed to the improvement in lift generation which brings once again an increase in the energy harvesting magnitude [24].…”
Section: Introductionmentioning
confidence: 99%
“…Another way to improve extraction efficiency can also be achieved by creating an effective camber which will produce a lift enhancement that is associated with the output power. This concept was studied by Bouzaher et al [29], who added a Gurney flap at the trailing-edge that when synchronized with the flapping motion at a Re = 1100 created this virtual camber that improved the output power. The lift production can be further improved by controlling the development of the leading-edge vortex than, when attached to the airfoil surface, contributed to the improvement in lift generation which brings once again an increase in the energy harvesting magnitude [24].…”
Section: Introductionmentioning
confidence: 99%
“…Bouzaher et al [27], added a gurney flap to the trailing edge of a flapping turbine at Re = 1100. When the motion of the GF synchronized with the flapping motion, a virtual camber was generated, which helped to improve the output power.…”
Section: Introductionmentioning
confidence: 99%
“…Modifications of the blade designs itself influence the performance of VAWTs. Different techniques have been used for boosting up the power coefficient (Cp) of H-Darrieus VAWT; such as deforming blades at leading edge [1] and trailing edge [2,3], using gurney flap [4] and flapped airfoil . Blade twist is also identified as a means for improving the VAWT's performance.…”
Section: Introductionmentioning
confidence: 99%