A study of the correlation between FSI flow behaviors and losses for the supersonic turbine cascade with millimeter-level ultra-thin blades and a high inlet flow angle
Fields of Study & Subjects
Computational Fluid Dynamics and Aerodynamics
Bladed Disk Vibration Dynamics
Turbomachinery Performance and Optimization
Publication details
- Journal / source
- Aerospace Science and Technology
- Publisher
- Elsevier BV
- Volume
- 172
- Pages
- 111700–111700
- Publication date
- 12 January 2026
- Language
- EN