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Effect of expanded hole on the aerodynamic and film cooli... | ResearchHub
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Effect of expanded hole on the aerodynamic and film cooling characteristics of turbine vane leading edge
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Authors
Xinnan Chen
4 more
Xinnan Chen
•
Bofeng Bai
2 more
•
Jun Li
Published
January 9, 2025
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Journal
Applied Thermal Engineering
Topics
Physics
Materials Science
Engineering
Aerospace Engineering
Mechanical Engineering
Show all topics
DOI
10.1016/j.applthermaleng.2025.125486
