ME-Programming-Final-Project---TurboJet-Analyis

This python tool can be used for analyzing turbojet cycle performance

$$ M = \frac{V}{\sqrt{\gamma R T}} $$

Name		Name	Last commit message	Last commit date
Latest commit History 15 Commits
.gitignore		.gitignore
README.md		README.md
combustor.py		combustor.py
compressor.py		compressor.py
diffuser.py		diffuser.py
engine.py		engine.py
graphs.py		graphs.py
gui.py		gui.py
node.py		node.py
nozzle.py		nozzle.py
plot_engine.py		plot_engine.py
turbine.py		turbine.py

Provide feedback