Transient Flow Evolution of a Hypersonic Inlet/Isolator with Incoming Windshear.
- Resource Type
- Article
- Source
- Aerospace (MDPI Publishing); Dec2023, Vol. 10 Issue 12, p1021, 20p
- Subject
HYPERSONIC flow WIND shear MACH number BOUNDARY layer (Aerodynamics) INLETS HYPERSONIC aerodynamics FLOW separation MOTION - Language
- ISSN
- 22264310