An accurate and rapid method for the design of supersonic nozzles

Ivan E. Beckwith, John A. Moore
naca-tn-3322
Feb 1955


A procedure is given for designing two-dimensional nozzles in which the streamline coordinates are computed directly from tabulated flow parameters and appropriate equations.

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http://naca.central.cranfield.ac.uk/reports/1955/naca-tn-3322.pdf