Design and Characterization of Mach 5 Flow for Highly Turbulent Hypersonic Test Facility
AIAA Scitech 2021 Forum
2021-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Mach 5 and Mach 8 hypersonic test facility
AIAA | 1989
|Hypersonic test facility Patent
NTRS | 1966
|Hypersonic test facility Patent
NTRS | 1967
|