Hypersonic flow scramjet
I want to know which solver will be good for solving hypersonic flow of Mach 8 with constant Cp and viscosity according to Sutherland's Law. No chemical reaction in the flow.
I tied sonicFoam but it's giving specieThermo error.
I also tried rhoCentralFaom but it's giving floating point exception.
|All times are GMT -4. The time now is 01:19.|