Design, Modeling, and Implementation of Nozzle and Diffuser Geometry for an Inductively Coupled Plasma Wind Tunnel Facility for Hypersonics and Magnetoaerodynamics
AIAA SCITECH 2024 Forum
01.01.2024
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Aerothermodynamic Design of an Inductively Coupled Plasma Wind Tunnel
British Library Conference Proceedings | 1997
|Nozzle/Diffuser For Test Section Of Wind Tunnel
NTRS | 1992
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