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turbine blade aerodynamic performance is improved
turbine blade aerodynamic performance is improved
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机译:涡轮叶片的空气动力学性能得到改善
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摘要
One or more protuberances are provided on a turbine blade on its suction side in a vicinity of its trailing edge. The protuberances serve to reduce a separation zone in a vicinity of a blade surface that is responsible for disturbances that affect efficiency of the turbine.
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