I am trying to build jet turbine examples for a class and I want to use actual values for the mass flow of fuel and air, combustion temps, exhaust temps, exhaust composition (CO, CO2,H20,o2, NOx) ext…
I thought this would be a quick 20 minutes of googling but I cant seem to find a clean consolidated source for the information.
I want to have the students run multiple scenarios showing a lean mix lowers the adiabatic flame temp and produced less NOx vs older designs that ran rich and had higher emissions rates. The values don’t need to be 100% accurate but in the ballpark would be nice. Links to sources would be best. Generic values used commonly in industry as back of a napkin values are a start.
I see that there are a lot of questions in the same ballpark of this but I (from my first run through) did not see one with all the information. Sorry if this is a repeat there are 1000’s of Questions on here to sift through.