Operating characteristics of 5° conical flow expander investigated in Lewis 2×2-ft Mach 3.88 tunnel to determine whether or not its use would establish full supersonic flow; results indicate that method should be practical.
Three-dimensional flow expander as device to increase Mach number in supersonic wind tunnel
NASA -- Memo
National Aeronautics and Space Administration -- Memorandums ; Memo n 10-6-58E
1958
7 pages
Report
English
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