Supersonic Nozzle Design Tool
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.
Cite As
Cory Dodson (2024). Supersonic Nozzle Design Tool (https://www.mathworks.com/matlabcentral/fileexchange/43212-supersonic-nozzle-design-tool), MATLAB Central File Exchange. Retrieved .
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