Vortex breakdown suppression in a compressor cascade using an l-shaped groove via flow deflection
Fields of Study & Subjects
Turbomachinery Performance and Optimization
Plasma and Flow Control in Aerodynamics
Combustion and flame dynamics
Publication details
- Journal / source
- Aerospace Science and Technology
- Publisher
- Elsevier BV
- Volume
- 172
- Pages
- 111709–111709
- Publication date
- 16 January 2026
- Language
- EN