MACH 4.3 AND 4.4 SUPERSONIC WIND TUNNEL FLOW WITH SUPERSONIC SINGLE AND DUAL INJECTION
Summary
MACH 4.3 AND 4.4 SUPERSONIC WIND TUNNEL FLOW WITH SUPERSONIC SINGLE AND DUAL INJECTION
NASA Identifier: GRC-C-1998-959
Tags
nasa
mach 4 3 and 4 4 supersonic wind tunnel flow with supersonic single and dual injection
dvids
high resolution
glenn research center
aviation research organization
Date
1998
Location
Source
Defense Visual Information Distribution Service
Link
Copyright info
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