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
2023-01-01
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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