Axisymmetric and Asymmetric Turbulent Shockwave Boundary Layer Interaction at Mach 2.5
AIAA AVIATION 2021 FORUM
01.01.2021
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Flow Field Measurements in a Crossing Shockwave Turbulent Boundary Layer Interaction at Mach 3
British Library Conference Proceedings | 1993
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