Mach Number 6 Capability for AEDC Supersonic Wind Tunnel (16S), Requirements and Concepts
24th, AIAA aerodynamic measurement technology and ground testing conference ; 2004 ; Portland, OR
2004-01-01
2494 pages
2004-2106 - 2004-2741 with gaps
Conference paper
English
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FEASIBILITY OF OPERATING THE AEDC SUPERSONIC WIND TUNNEL (16S) UP TO MACH NUMBER 6
British Library Conference Proceedings | 2004
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