About this document
Compressible Flow Nozzle Analysis by Mubarak Kazmin is a document available to read on EtoBox.
This document discusses a fluid dynamics laboratory experiment on compressible flow through a nozzle. The experiment involves measuring pressure and calculating Mach number at the throat of a nozzle where the pressure ratio reaches 0.528 and flow becomes sonic or supersonic downstream. Graphs are produced showing pressure distribution along the nozzle where shock waves are observed when flow becomes supersonic. Sensitivities of measurement tools like barometers and rotameters are also noted.
- Author
- Mubarak Kazmin
- Language
- EN