I've been trying to simulate flow conditions at 100 km altitude over a re entry capsule in fluent.
Conditions are
Temperature:
168.7219
K
Density = 0.000000577 Kg/m3
Pressure = 0.0289 N/m2
I tried using laminar and k-w model. The solution does not converge even after 50000 iterations using the density based solver and ideal gas equation.
Is there a way to go about it?
Please let me know.