[neerajpdh]

Hello
This is a combustion problem. (laminar, species transport model) I would like to give the mass flux at the inlet boundary which is a function of heat flux at the inlet boundary. This heat flux must be calculated internally by fluent due to combustion.
mass flux in (kg/m^2 sec) = q(watts/m^2)*a + b, where a and b are some fitting constants from a relation.

I am new to fluent, someone pls guide me in this regard.
Thanks in advance.