Investigation on the effect of hole diameter and wall thickness on the overall cooling effectiveness of turbine vane leading edge

Wang, Rui; Ye, Lin; Zhang, Lingjun; Liu, Cunliang; Cao, Feifei; Hui, Zhonghao

doi:10.1016/j.applthermaleng.2024.122662

Applied Thermal Engineering

2024

DOI: 10.1016/j.applthermaleng.2024.122662

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Investigation on the effect of hole diameter and wall thickness on the overall cooling effectiveness of turbine vane leading edge

Rui Wang,

Lin Ye,

Lingjun Zhang

et al.

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Study on the recovery temperature and overall cooling effectiveness of the different profiles of the blade under the condition of non-uniform turbine inlet temperature

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et al. 2025

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Study on effects of inlet nonuniformities on aerothermal performance of NGV pressure side with different film cooling designs

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Investigation on the effect of hole diameter and wall thickness on the overall cooling effectiveness of turbine vane leading edge

Cited by 2 publications

References 20 publications

Study on the recovery temperature and overall cooling effectiveness of the different profiles of the blade under the condition of non-uniform turbine inlet temperature

Study on the recovery temperature and overall cooling effectiveness of the different profiles of the blade under the condition of non-uniform turbine inlet temperature

Study on effects of inlet nonuniformities on aerothermal performance of NGV pressure side with different film cooling designs

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