Film cooling performance of turbine blade leading edge with internal return-flow impingement cooling scheme

Applied Thermal Engineering 2026

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Authors: Nan Xu, Han Yan, Lei Luo, Wei Du, Licheng Guo
DOI: 10.1016/j.applthermaleng.2026.129930
Cited by: 1
References: 36

Fields of Study & Subjects

Heat Transfer Mechanisms Turbomachinery Performance and Optimization Bladed Disk Vibration Dynamics

Publication details

Journal / source
Applied Thermal Engineering
Publisher
Elsevier BV
Volume
289
Pages
129930–129930
Publication date
24 January 2026
Language
EN