Numerical Study of Shock-Wave/Boundary-Layer Interaction Control Using Variable Pressure and Inlet Size
Fields of Study & Subjects
Computational Fluid Dynamics and Aerodynamics
Plasma and Flow Control in Aerodynamics
Combustion and Detonation Processes
Publication details
- Journal / source
- Lecture notes in mechanical engineering
- Pages
- 277–290
- Publication date
- 1 January 2026
- Language
- EN