DEVELOPMENT OF A DIRECT-CONNECT TESTING CAPABILITY IN THE HYPERTERP SHOCK TUNNEL
AIAA SciTech Forum and Exposition ; 2021 ; Online
Ground testing ; 273-285
2021
Aufsatz (Konferenz)
Englisch
TECHNICAL NOTES Unstarted Inlet for Direct-Connect Combustor Experiments in a Shock Tunnel
Online Contents | 2000
|Closed-Loop Control of Shock Location in Mach 1.8 Direct Connect Wind Tunnel (AIAA 2014-2935)
British Library Conference Proceedings | 2014
|