The installation and performance evaluation of a small supersonic wind tunnel system

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Author
Brown, Charles O.
Date
1961Advisor
Howard, Charles P.
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Show full item recordAbstract
This report describes the procedure utilized in the assembly and
evaluation of a small intermittent blowdown supersonic wind tunnel.
The tunnel proper was fully constructed and nozzle blocks for
attainment of a Mach number of 1.5 or 2.37 in the 1/2" by 1.718"
test section were available. The basic schlieren system was purchased
complete. An attempt was made to use or convert readily available
materials for all components.