Convective Burning Droplet Model for Liquid Rocket Combustion Chambers
Channel: ErnestYAlumni
Date: 2016-03-15

Simple model of a Convective Burning Droplet for Liquid Rocket Combustion Chamber; for fuel, I used methane (CH4) and n-heptane (C7H16).  For oxidizer, I used (liquid) oxygen (O2 or LOX).  cf. Stephen Turns, An Introduction to Combustion: Concepts and Applications. 3rd. Ed. McGraw-Hill (2011).  

github: ernestyalumni/Propulsion/ccdroplet