Hypersonic boundary layer instability measurements at Mach 7 and flight total enthalpy
This paper presents boundary layer instability measurements obtained in The University of Queensland’s T4 Stalker Tunnel at Mach 7. The model geometry is a 7◦ half angle cone with a nose bluntness of 1.55 mm radius, pitched at an angle of attack of zero degrees. Results are presented at a constant e...
Main Authors: | , , , |
---|---|
Format: | Conference item |
Language: | English |
Published: |
2019
|