Geometric evolution and cooling performance degradation of film cooling holes under long-term ablation in advanced gas turbines

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Authors: Kun DU, Y X Liu, Y X Liu, Min XIA, Kunyang Li, Fangshun Zhang, Cunliang Liu
Cited by: 5
References: 44

Fields of Study & Subjects

Turbomachinery Performance and Optimization Heat Transfer Mechanisms Computational Fluid Dynamics and Aerodynamics

Publication details

Journal / source
Aerospace Science and Technology
Publisher
Elsevier BV
Volume
172
Pages
111716–111716
Publication date
14 January 2026
Language
EN