[gokenq]

Hi all,

currently, I am working on a high-altitude reentry 2D Axisymmeritc simulation, and I couldn't figure out the right setup on in the fluent. Would anyone help me out with this? Thank you!

My target condition is following:
Mach = 3.0
Vel = 960.0 m/s
T = 254.6 K
Re/m = 37769.8 (note how low this is)
Rho = 0.000643 kg/m3

and my current setup are :
Velocity speed (960 m/s )
initial pressure (52 pa for high altitude )
material: air
density: ideal gas
viscosity: Sutherland law
energy: on (automatic for ideal gas)
wall: slip wall with 0 shear
Solver: Density-based
BC: pressure farfield with Mach 3 speed

[Kummi]

Have you run this above case setup and faced any errors ?