Cooling methods for gas turbine blade leading edge:...

International Communications in Heat and Mass Transfer 2019 / 01 Vol. 100

Cooling methods for gas turbine blade leading edge: Comparative study on impingement cooling, vortex cooling and double vortex cooling

Fan, Xiaojun, Li, Liang, Zou, Jiasheng, Zhou, Yuanyuan
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Volume:
100
Language:
english
Journal:
International Communications in Heat and Mass Transfer
DOI:
10.1016/j.icheatmasstransfer.2018.12.017
Date:
January, 2019
File:
PDF, 6.71 MB
english, 2019
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