MACH 4.3 SUPERSONIC WIND TUNNEL FLOW WITH DUAL SUPERSONIC AND / OR SINGLE FLOOR INJECTION USING POSITIVE 50 DIOPTER SHADOWGRAPH SYSTEM CORRECTION
Summary
MACH 4.3 SUPERSONIC WIND TUNNEL FLOW WITH DUAL SUPERSONIC AND / OR SINGLE FLOOR INJECTION USING POSITIVE 50 DIOPTER SHADOWGRAPH SYSTEM CORRECTION
NASA Identifier: C-1998-1283
Nothing Found.
Tags
nasa
mach 4 3 supersonic wind tunnel flow with dual supersonic and or single floor injection using positive 50 diopter shadowgraph system correction
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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