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This study can be useful in turbine blade cooling design.
为涡轮叶片的冷却结构设计提供了依据。
youdao
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The cooling effectiveness of pressure side of blade was higher than suction side.
层板叶片压力面的冷效略高于吸力面。
youdao
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The cooling effectiveness of pressure side of blade was higher than suction side.
层板叶片压力面的冷效略高于吸力面。
youdao