Enabling Advanced Wind-Tunnel Research Methods Using the NASA Langley 12-Foot Low Speed Tunnel
14th AIAA Aviation Technology, Integration, and Operations Conference
01.01.2014
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2014
|NASA Langley Mach 6 Quiet Wind-Tunnel Performance
AIAA | 1997
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