A MATLAB code incorporating the analysis method described by Barrowman (1967) to analyse the aerodynamic properties of a supersonic sounding rocket.
-
Updated
Jun 28, 2022 - MATLAB
A MATLAB code incorporating the analysis method described by Barrowman (1967) to analyse the aerodynamic properties of a supersonic sounding rocket.
Add a description, image, and links to the supersonic-flow topic page so that developers can more easily learn about it.
To associate your repository with the supersonic-flow topic, visit your repo's landing page and select "manage topics."