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Old   March 26, 2013, 09:37
Default Doubts regarding cfd fluent
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swathy09 is on a distinguished road
I started a project on hypersonic speeds.Im new to the software and iv got doubts regarding the boundary trying to obtain the characteristics of a blunt body at mach 7.but every-time i plot, my cd range shoots up to 30000 and more,and shock is not captured either.Can anyone help me with the boundary condition?
Boundary Conditions:
density based solver
operating pressure 1atm
temperature 2236k
gauge pressure: 1.79979e08
pressure inlet and n pressure outlet condition
n i used k-epsilon.
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