The Experiments and Stability Analysis of Hypersonic Boundary Layer Transition on a Flat Plate.
- Resource Type
- Article
- Source
- Applied Sciences (2076-3417); Dec2023, Vol. 13 Issue 24, p13302, 14p
- Subject
BOUNDARY layer (Aerodynamics) MACH number WIND tunnels REYNOLDS number TEMPERATURE distribution - Language
- ISSN
- 20763417