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Numerical study on a modified impulse turbine for OWC wave energy conversion
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文摘

A modified impulse turbine within rotor blade setting angle is proposed for asymmetrical air flow velocity amplitude conditions.

Numerical model is set up based on Fluent and validated by corresponding experimental data.

Flow field and pressure distribution around the rotor blade are illustrated.

Mean efficiency in a wave cycle demonstrates that a 5° setting angle of rotor blade is optimum for the inhalation to exhalation velocity amplitude ratio 0.6.

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