Development of a Direct-Connect Testing Capability in the HyperTERP Shock Tunnel
AIAA Scitech 2021 Forum
01.01.2021
Aufsatz (Konferenz)
Elektronische Ressource
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
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