About this document
Aerolab II Report 2 by ae23b102 is a document available to read on EtoBox.
The document outlines an experiment aimed at determining the position of shock waves in a compressible flow setup using a converging-diverging nozzle. It details the apparatus used, the theory behind choked flow, observations of pressure distributions, sources of error, and concludes that the shock location shifts downstream as back pressure is varied. Additionally, it includes Python code for plotting static pressure against area ratio.
- Author
- ae23b102
- Language
- EN