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A new numerical method for predicting the profile loss of turbine blades in subsonic and supersonic flows is presented.
给出了一个计算亚、跨音涡轮叶栅叶型损失的数值计算方法。
youdao
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A new numerical method for predicting the profile loss of turbine blades in subsonic and supersonic flows is presented.
给出了一个计算亚、跨音涡轮叶栅叶型损失的数值计算方法。
youdao