Liquefaction of air in the Langley 11-inch hypersonic tunnel

Charles H. McLellan, Thomas W. Williams
naca-tn-3302
Oct 1954


Pressure and scattered-light measurements were made in the Langley 11-inch hypersonic tunnel to determine the effect of stagnation temperature on the flow in two Mach number 7 nozzles and to determine the nature of the condensation process occurring at low stagnation temperatures.

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