The internal coolant channel in an actual turbine blade was simplified into a variable cross-section channel with ribs and bleeding holes.

  • 以航空发动机涡轮叶片中段内部冷却通道为研究对象,将其简化为带肋变截面U型通道。

  • 互联网摘选 2025-01-20 11:40:27

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