DUCT LAB SUPERSONIC WIND TUNNEL MACH 4.3 PLUS FLOW WITH AND WITHOUT DUAL AIR INJECTION
Summary
DUCT LAB SUPERSONIC WIND TUNNEL MACH 4.3 PLUS FLOW WITH AND WITHOUT DUAL AIR INJECTION
NASA Identifier: C-1998-492
Tags
nasa
duct lab supersonic wind tunnel mach 4 3 plus flow with and without dual air injection
dvids
high resolution
glenn research center
aviation research organization
wind tunnel
engineering
Date
1998
Location
Source
Defense Visual Information Distribution Service
Link
Copyright info
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