2001
DOI: 10.1016/s0960-1481(00)00175-0
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A review of impulse turbines for wave energy conversion

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Cited by 200 publications
(147 citation statements)
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“…The inlet/outlet angle γ of the rotor is 60 degrees and the setting angle θ of the guide vane is 30 degrees. The turbine configuration was adopted on the basis of the air turbine test results [16]. …”
Section: Experimental Apparatusmentioning
confidence: 99%
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“…The inlet/outlet angle γ of the rotor is 60 degrees and the setting angle θ of the guide vane is 30 degrees. The turbine configuration was adopted on the basis of the air turbine test results [16]. …”
Section: Experimental Apparatusmentioning
confidence: 99%
“…Setoguchi et al [16,17] reviewed a variety of experimental results concerning the performances of the Wells turbine and the impulse turbine. Takao et al [18] show that the impulse turbine with a fixed guide vane was superior to the Wells turbine in the actual sea with irregular waves.…”
Section: Introductionmentioning
confidence: 99%
“…The airflow is reciprocating in nature. The turbine rotates in one direction irrespective of the airflow direction (Setoguchi, Santhakumar, Maeda, Takao, & Kaneko, 2001). Hence, it is called a bidirectional turbine or bidirectional flow turbine.…”
Section: Introductionmentioning
confidence: 99%
“…As concerns the secondary conversion, by means of the test rig having a piston-cylinder to generate the oscillating air flow, the performance of the air turbine was evaluated in a series of studies. Setoguchi et al [9,10] reviewed a variety of experimental results concerning the performances of the Wells turbine and the impulse turbine. Besides, Takao et al [11] showed that the impulse turbine was superior to the Wells turbine in a wide flow rate range.…”
Section: Introductionmentioning
confidence: 99%
“…4 shows the basic configuration of the rotor and the fixed guide vanes. This turbine configuration was adopted on the basis of the air turbine test results [9]. The numbers of the rotor blades and the single-stage guide vanes are 30 mm, the hub ratio  is 0.7 and the clearance between the rotor blade tip and the casing is 0.3 mm.…”
Section: Introductionmentioning
confidence: 99%