A Study of Potential Test Capabilities of the NASA Langley 0.3-Meter Transonic Cryogenic Wind Tunnel
30th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
2014-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Application of FLEET Velocimetry in the NASA Langley 0.3-meter Transonic Cryogenic Tunnel
British Library Conference Proceedings | 2015
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