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