Hey guys, I am currently doing research on fuels for 'fire safe' aviation. As part of my project I will set up some modeling approaches for the injection of fuel into the combustion 'chamber' (jet engines).
Unfortunately I have not been able to find reliable information on this process. I would need the following information (for large jet aircraft and standard engine performance):
- the pressure difference from the nozzle to the chamber
- the fuel temperature at injection
- the common nozzle type (length and diameter)
Of course there are various values for various aircraft but any of those would potentially help me (e.g. Boeing 737). Also ideally you would send me a link or official statement of the above mentioned things.
Hope I can get some pointers in the right direction.