Control of Cowl Shock/Boundary Layer Interaction in Supersonic Inlet Based on Dynamic Vortex Generator.
- Resource Type
- Article
- Source
- Aerospace (MDPI Publishing); Aug2023, Vol. 10 Issue 8, p729, 26p
- Subject
BOUNDARY layer (Aerodynamics) BOUNDARY layer separation VORTEX generators SUPERSONIC flow FLOW separation SWIRLING flow SHOCK waves - Language
- ISSN
- 22264310