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
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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