HYPERSONIC SLENDER-CONE BOUNDARY-LAYER INSTABILITY IN THE UMD HYPERTERP SHOCK TUNNEL
AIAA SciTech Forum and Exposition ; 2020 ; Orlando, Fla.
Fluid dynamics ; Volume 2 of 7 ; 995-1008
2020
Aufsatz (Konferenz)
Englisch
Hypersonic Wind-Tunnel Measurements of Boundary-Layer Transition on a Slender Cone
Online Contents | 2016
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