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
2024-01-01
Conference paper
Electronic Resource
English
Nozzle/Diffuser For Test Section Of Wind Tunnel
NTRS | 1992
|Aerothermodynamic Design of an Inductively Coupled Plasma Wind Tunnel
British Library Conference Proceedings | 1997
|