NASA NTRS · 19700049883
Viscous effects on the flow coefficient for a supersonic nozzle
Abstract
Adiabatic flow coefficient in supersonic nozzle with choked flow conducted over throat Reynolds number range
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Back, L. H., Massier, P. F., Noel, M. B., Saheli, F.. 1970-03-01. Viscous effects on the flow coefficient for a supersonic nozzle. https://ntrs.nasa.gov/citations/19700049883
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