This study can be useful in turbinebladecooling design.
为涡轮叶片的冷却结构设计提供了依据。
2
The experimental results are valuable reference for aero-engine turbinebladecooling designers.
本文的实验结果对于航空发动机涡轮叶片冷却结构设计具有参考价值。
3
This essay analyzes the cooling principle and the mode of operation of the M701F gas turbinebladecooling technology to verify its efficiency in enhancing the safety of the gas turbine.