Supersonic Nozzle Design Tool

Versione 1.1.0.0 (3,54 KB) da Cory Dodson
Outputs rectangular nozzles based on 2-D, inviscid method of characteristics.
4.8
(9)
4,3K download
Aggiornato 7 mag 2014

Visualizza la licenza

Employs inviscid, 2-D method of characteristics for rectangular cross-sections to develop geometry for the diverging section of a supersonic nozzle.
The code presented here was used to develop nozzle geometry for a supersonic wind tunnel, which has been fabricated, tested, and verified.

Note: Non-physical geometry presents when the too many Mach waves are specified. This is thought to be the result of the more extreme slope that results from specifying a greater number of Mach lines.

Cita come

Cory Dodson (2026). Supersonic Nozzle Design Tool (https://it.mathworks.com/matlabcentral/fileexchange/43212-supersonic-nozzle-design-tool), MATLAB Central File Exchange. Recuperato .

Compatibilità della release di MATLAB
Creato con R2013a
Compatibile con qualsiasi release
Compatibilità della piattaforma
Windows macOS Linux
Categorie
Scopri di più su Thermal Analysis in Help Center e MATLAB Answers
Tag Aggiungi tag
Open in new tab
Versione Pubblicato Note della release
1.1.0.0

Updated description to be more specific. Also updated files to latest version on computer. These may not have changed since last update.
1.0.0.0