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...
| Autors principals: | , , , |
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| Format: | Conference item |
| Idioma: | English |
| Publicat: |
2019
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