GitHub - z-devin/Ramjet_Engine_Design: Airbreathing ramjet engine design and analysis for ME-433 Rocket Science independent study. Models inlet oblique shocks, Method of Characteristics nozzle design, Rayleigh combustion, and control volume thrust analysis for Mach 2.75-3.25 operation at 50,000 ft.

Branches Tags

Name		Name	Last commit message	Last commit date
Latest commit History 85 Commits
Ramjet_Design		Ramjet_Design
Tools		Tools
.gitignore		.gitignore
Ramjet_Engine_Design_Report.pdf		Ramjet_Engine_Design_Report.pdf
Rocket_Midterm.ipynb		Rocket_Midterm.ipynb
airfoil.py		airfoil.py
converging_section.py		converging_section.py
expansion_wave.py		expansion_wave.py
moc_nozzle.py		moc_nozzle.py
nozzle.py		nozzle.py
oblique_shock.py		oblique_shock.py
standard_atmosphere_1976.py		standard_atmosphere_1976.py
wind_tunnel.py		wind_tunnel.py

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Airbreathing ramjet engine design and analysis for ME-433 Rocket Science independent study. Models inlet oblique shocks, Method of Characteristics nozzle design, Rayleigh combustion, and control volume thrust analysis for Mach 2.75-3.25 operation at 50,000 ft.