Supersonic Nozzle Design Tool
Outputs rectangular nozzles based on 2-D, inviscid method of characteristics.
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.
引用格式
Cory Dodson (2026). Supersonic Nozzle Design Tool (https://ww2.mathworks.cn/matlabcentral/fileexchange/43212-supersonic-nozzle-design-tool), MATLAB Central File Exchange. 检索时间: .
