Investigation of the use of the thermal decomposition of nitrous oxide to produce hypersonic flow of a gas closely resembling air

Alexander P. Sabol, John S. Evans
naca-tn-3624
Mar 1956


During the tests, measurement were made of the stagnation pressure in the settling chamber and of the static pressures at 10 stations located in a spiral fashion along the conical nozzle wall at intervals of approximately 6.4 millimeters.

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