
NOZZLE 1.0
Latest version:
1.0
See all
Developer:
AeroRocket
Nozzle is a one-dimensional with cross-sectional area variation, compressible flow computer program for the analysis of converging-diverging nozzles. Nozzle internal flow may be entirely subsonic, entirely supersonic or a combination of subsonic and supersonic including shock waves in the diverging part of the nozzle.
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