Design and Viscous Correction of an Axisymmetric Contoured Nozzle for Perfect Gas to the T2 Hypersonic Shock Tunnel
25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
01.01.2023
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Axisymmetric Simulation of Turbulent Hypersonic Flows in Contoured Nozzle
British Library Conference Proceedings | 2013
|Condensation in a contoured-nozzle shock tunnel
AIAA | 1970
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