2011
DOI: 10.1016/j.apor.2011.07.002
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Numerical investigation on the performance of Wells turbine with non-uniform tip clearance for wave energy conversion

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Cited by 57 publications
(22 citation statements)
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“…Taha et al [27] reported a uniform TC with different chord length ratios. Although a non-uniform TC has a better performance [9], the manufacturing difficulty may arise.…”
Section: Introductionmentioning
confidence: 99%
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“…Taha et al [27] reported a uniform TC with different chord length ratios. Although a non-uniform TC has a better performance [9], the manufacturing difficulty may arise.…”
Section: Introductionmentioning
confidence: 99%
“…Efforts have been made to increase the performance of the Wells turbine by changing duct geometry [2], designing monoplane and biplane Wells turbine [3], optimizing blade profile and thickness [4], modifying airfoil profile [5e7], making non-symmetric airfoil blade shape [8] and non-uniform tip gap [9], inserting end plate [10], sweeping [11,12], changing blade pitch angle [13,14], etc. Other efforts involve modification of guide vane angle [15e17], bidirectional flow [18], variable chord [19], bi-plane unidirectional blade [20], counter rotating blade [21,22], hysteretic behavior with unsteady flow [23], etc.…”
Section: Introductionmentioning
confidence: 99%
“…A large number of W-T CFD models relied on solutions of the steady averaged Navier-Stokes equation [37,113,139,140]. A large number of W-T CFD models relied on solutions of the steady averaged Navier-Stokes equation [37,113,139,140].…”
Section: Cfd Modeling Goals Of W-tmentioning
confidence: 99%
“…The experimental work is performed at a test rig capable of producing reversing air flows. Many of CFD investigations employ this experimental work as a validation case such as T. H. Kim, et al [76,113] and Zahari Taha, et al [139,140], in addition to several other CFD works in [77,81,82,129,134,135]. The piston can be driven back and forth by means of three ball screws acted upon by a DC servomotor.…”
Section: Validation Of Cfd Modelsmentioning
confidence: 99%
“… studied the effect of the blade aspect ratio and the rotor hub‐to‐tip ratio on the performance of Wells turbines. Authors have also investigated other geometrical parameters like the effect of inlet guide vanes , blade setting angle , end plates , and tip clearance . Shaaban and Abdel Hafiz presented numerical optimization of the Wells turbine duct geometry.…”
Section: Introductionmentioning
confidence: 99%