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Investigation of pressure surface film cooling of the turbine vane considering the strong swirl characteristics at the combustor exit

Xiaohui Bai, Yingjie Du, Helong Jin, Zhong-yi Fu, Xian‐Long Meng, Cunliang Liu

2025Applied Thermal Engineering10 citationsDOI

Topics & Concepts

CombustorTurbineMaterials scienceGas turbinesMechanicsTurbine bladeCombustion chamberMechanical engineeringEngineeringCombustionPhysicsOrganic chemistryChemistryCombustion and flame dynamicsTurbomachinery Performance and OptimizationHeat Transfer Mechanisms
Investigation of pressure surface film cooling of the turbine vane considering the strong swirl characteristics at the combustor exit | Litcius