Hello there!
I am working as a fun-project on simulating rocket engine conditions in cantera with cryogenic propellants, which to no ones surprise, it is quite challenging. First of all, I have simplified the problem to a 1D counterflow H2/O2 diffusion flame and I have even implemented the Peng-Robinson equation of state. However, there is one major problem that I can get over with. The flames from the papers I have chosen to validate the real-gas model (Lacaze 2012 and Banuti 2018) both have inlet temperatures of 125K and cantera will not simulate under 200K.
I have looked at the source code. On one side, there is the polynomial parametrization of thermodynamic values in h2o2.yaml that are validated at temperatures upwards of 200K, but changing the lower limit does not seem to change anything. On the other side, I have tried to look other places where a hard cap at T=200K might have been implemented but it has not granted any result.
For this reason, I was wandering if anyone knows how can I sumilate such flames at temperatures lower than 200K and how I can do it.
Thanks in advance,
Xavi