Effect of Surface Deformation on Hypersonic Transitional Shock-Wave/Boundary-Layer Interactions on the ROTEX-T Cone-Flare
AIAA SCITECH 2025 Forum
01.01.2025
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Transitional Shock Wave-Boundary Layer Interaction over a Cone Flare Model at Hypersonic Conditions
British Library Conference Proceedings | 2002
|Transitional shock wave boundary layer interactions in hypersonic flow
British Library Conference Proceedings | 2003
|