FEASIBILITY OF OPERATING THE AEDC SUPERSONIC WIND TUNNEL (16S) UP TO MACH NUMBER 6
42nd:; Meeting, Aerospace sciences; 42nd AIAA aerospace sciences meeting and exhibit ; 2004 ; Reno, NV
2004-01-01
AIAA 2004-1138
AIAA 2004-0001 - AIAA 2004-1388 held with gaps
Conference paper
English
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Mach Number 6 Capability for AEDC Supersonic Wind Tunnel (16S), Requirements and Concepts
British Library Conference Proceedings | 2004
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