Check for inlet temperature
Following procedure could be used to compute specified input temperature at an inlet from simulation results. The procedure could be used after proper convergence is achieved in a case which has heat transfer and doesn't involve either radiative heat transfer or combustion.
Specific_Heat_at _Constant_Pressure (Cp):
Report--->Surface Integrals--->Facet Average--->Properties--->Specific Heat
T = [ Q/ (Cp*M) ] + 298.15 kelvin